While palying with the Talent Queue I managed to chock up 1300 days of training, just to see how it worked.... erm... it'd be nice if there was a "Clear Queue" button as I've crashed out once while clearing out the queue. And yes, you need to pretty much start from the bottom and work your way up due to dependencies.
While palying with the Talent Queue I managed to chock up 1300 days of training, just to see how it worked.... erm... it'd be nice if there was a "Clear Queue" button as I've crashed out once while clearing out the queue. And yes, you need to pretty much start from the bottom and work your way up due to dependencies.
NQ: "Oh no, you've got level 3 in most refining and smelting and almost was tier 3 at all industry but that's worth absolutely nothing because today, today we've lost our freakin' minds and opted to make you train that industry ALL OVER AGAIN and dump HUNDREDS of MILLIONS of credits into the market just to make the same stuff you could make and skilled up to make faster and more efficiently yesterday."
Honestly. Yesterday I could happily build ship parts to build ships to build blueprints to give away for free. Yes, I run FELD.
Today, I have to not only buy schematics for everything I need to build to build ships, but I also need to "train up" to the correct level of industry to actually build the schematic. And to refine ore. And to smelt the actual mats to make the parts. PICK ONE! Either train or schematics. I am being punished for wanting to design and build ships now. I'd not minded schematics as that didn't require me to work with the terrible training queue. (Move to TOP/Highest Possible button please!). Now I need to fish through the markets, spend what little UEC I have, and hope I can find what I need to continue making free and better (yep, no design is perfect) designs for FELD.
But NQ did both. Which is pretty lame since TRAINING only slows down industrial player's OTHER training by about 3 months so they can train in the higher tiers of... industry. If NQ wanted to stop everyone training for 3 months then NQ should have just paused everyone's training queue for 3 months.
AND WHERE IS THE PUNISHMENT FOR THE MINERS? Really - they just OCD raw ores all day with ZERO cost and ZERO need for industry. They have ZERO training to do to know how to mine ores. They have ZERO things to buy to actually mine the ores. They just sit back and reap profits. That's been my biggest beef with this whole thing - miners have strip mined almost ever l of t3+ ore out using multi-boxing to run multiple scanning rigs and mining alts that the prez of NQ ENCOURAGES PEOPLE TO DO. If I want to get T3+ ore via mining as a single boxer I am forced to scan areas in hopes I can find something that strip miners have missed or deemed "not worth their effort."
Toss in that this just means multi-boxers just need to set their alts to train the new skills and wow, no way for any soloist to compete even as a niche industrialist.
Well thank you, NQ. It all adds up to a major excuse not to play. I am debating just not playing. I liked to build stuff and give away the designs but now it's just work and doing what I hate most - WAITING for something that should be nothing to get done.
The only gameplay I am thinking about doing now is scrapping everything, freighting it all to my plot on Sanct, and uninstalling. Industry is just to punitive now.
I might revisit in a few months to see if NQ came to some form of reality.
NQ: "Oh no, you've got level 3 in most refining and smelting and almost was tier 3 at all industry but that's worth absolutely nothing because today, today we've lost our freakin' minds and opted to make you train that industry ALL OVER AGAIN and dump HUNDREDS of MILLIONS of credits into the market just to make the same stuff you could make and skilled up to make faster and more efficiently yesterday."
Honestly. Yesterday I could happily build ship parts to build ships to build blueprints to give away for free. Yes, I run FELD.
Today, I have to not only buy schematics for everything I need to build to build ships, but I also need to "train up" to the correct level of industry to actually build the schematic. And to refine ore. And to smelt the actual mats to make the parts. PICK ONE! Either train or schematics. I am being punished for wanting to design and build ships now. I'd not minded schematics as that didn't require me to work with the terrible training queue. (Move to TOP/Highest Possible button please!). Now I need to fish through the markets, spend what little UEC I have, and hope I can find what I need to continue making free and better (yep, no design is perfect) designs for FELD.
But NQ did both. Which is pretty lame since TRAINING only slows down industrial player's OTHER training by about 3 months so they can train in the higher tiers of... industry. If NQ wanted to stop everyone training for 3 months then NQ should have just paused everyone's training queue for 3 months.
AND WHERE IS THE PUNISHMENT FOR THE MINERS? Really - they just OCD raw ores all day with ZERO cost and ZERO need for industry. They have ZERO training to do to know how to mine ores. They have ZERO things to buy to actually mine the ores. They just sit back and reap profits. That's been my biggest beef with this whole thing - miners have strip mined almost ever l of t3+ ore out using multi-boxing to run multiple scanning rigs and mining alts that the prez of NQ ENCOURAGES PEOPLE TO DO. If I want to get T3+ ore via mining as a single boxer I am forced to scan areas in hopes I can find something that strip miners have missed or deemed "not worth their effort."
Toss in that this just means multi-boxers just need to set their alts to train the new skills and wow, no way for any soloist to compete even as a niche industrialist.
Well thank you, NQ. It all adds up to a major excuse not to play. I am debating just not playing. I liked to build stuff and give away the designs but now it's just work and doing what I hate most - WAITING for something that should be nothing to get done.
The only gameplay I am thinking about doing now is scrapping everything, freighting it all to my plot on Sanct, and uninstalling. Industry is just to punitive now.
I might revisit in a few months to see if NQ came to some form of reality.
I can't even get NQ to clean up my neighbors racist slurs. I am surprised they even took a stand on everything. I logged a ticket, even went to the discord and tried to get a tech to do something. He just said "it will be taken care of" and then blew me off by saying "it was the end of his shift." I am about to send the stuff to a friend so he can take it to the courts of reddit how DU allows racist slurs and harassments with said slurs.
So with all that being said I am surprised NQ did anything about the ship jacking.
Everyone knows bigger guns are better guns when it comes to DPS and DU is no exception. Currently the mechanics of DU are as follows:
- Hoover seats and cockpits can only use XS guns.
- Command seats can't use weapons
- Gunner seats are limited to their size and below. S gunner seats can use S and XS weapons, M gunner seats can use M, S, and XS weapons, etc
That being said it is pretty obvious where the pay to win aspect comes into play for PvP. Those who pay extra for an entirely new PC and a sub account can multi-box. Multi-boxing is not banned or discouraged by NQ based on this interview:
https://www.youtube.com/watch?v=ai3Kk37ntgg
Essentially anyone who does mult-iboxing can run both the pilot seat and the gunner seat at the same time. You just need a twisty joystick or pedal setup to do so. MB's don't need to fly all that well - they just need to keep guns facing the target. MB's just need to be able to shoot half way decent and that is it.
With the current "it fits, it ships" methodology of DU players can shove as large guns as they can afford onto their ship. With multi-boxing this means a solo player who is there to enjoy the game with his one computer will be out matched by the multi-boxer. Add in the "fluid" aka safe zone border exploits that allow attackers to shoot at defenseless ships in the safe zone which people who see no issues with the current multiboxing advantage will happily exploit.
It's pay to win in the current state of the game - if you consider PvP victories a win state.
Everyone knows bigger guns are better guns when it comes to DPS and DU is no exception. Currently the mechanics of DU are as follows:
- Hoover seats and cockpits can only use XS guns.
- Command seats can't use weapons
- Gunner seats are limited to their size and below. S gunner seats can use S and XS weapons, M gunner seats can use M, S, and XS weapons, etc
That being said it is pretty obvious where the pay to win aspect comes into play for PvP. Those who pay extra for an entirely new PC and a sub account can multi-box. Multi-boxing is not banned or discouraged by NQ based on this interview:
https://www.youtube.com/watch?v=ai3Kk37ntgg
Essentially anyone who does mult-iboxing can run both the pilot seat and the gunner seat at the same time. You just need a twisty joystick or pedal setup to do so. MB's don't need to fly all that well - they just need to keep guns facing the target. MB's just need to be able to shoot half way decent and that is it.
With the current "it fits, it ships" methodology of DU players can shove as large guns as they can afford onto their ship. With multi-boxing this means a solo player who is there to enjoy the game with his one computer will be out matched by the multi-boxer. Add in the "fluid" aka safe zone border exploits that allow attackers to shoot at defenseless ships in the safe zone which people who see no issues with the current multiboxing advantage will happily exploit.
It's pay to win in the current state of the game - if you consider PvP victories a win state.
09/27 Changed math from U.S. tons to tonnes. 907.185 -> 1000
10/07 Updated svg bootstrap and ADDED MasterOfAll's Newer Version.
NEW VERSION MADE BY MasterOfAll
Features
Time till Destination = TTD
Displays Destination that was chosen.
Does Speed displayed as Velocity
Comes with Sleek White Buttons.
Pasteable Form Here Just Paste to PB and Link Screen and Core.
{"slots":{"0":{"name":"screen","type":{"events":[],"methods":[]}},"1":{"name":"core","type":{"events":[],"methods":[]}},"2":{"name":"slot3","type":{"events":[],"methods":[]}},"3":{"name":"slot4","type":{"events":[],"methods":[]}},"4":{"name":"slot5","type":{"events":[],"methods":[]}},"5":{"name":"slot6","type":{"events":[],"methods":[]}},"6":{"name":"slot7","type":{"events":[],"methods":[]}},"7":{"name":"slot8","type":{"events":[],"methods":[]}},"8":{"name":"slot9","type":{"events":[],"methods":[]}},"9":{"name":"slot10","type":{"events":[],"methods":[]}},"-1":{"name":"unit","type":{"events":[],"methods":[]}},"-2":{"name":"system","type":{"events":[],"methods":[]}},"-3":{"name":"library","type":{"events":[],"methods":[]}}},"handlers":[{"code":"MapScreenMouseX = x\nMapScreenMouseY = y\nMapScreenMouseDown = false\nlocal buttonNo = evaluateButtons()\nif MapScreenButtonSelected > 0 and MapScreenButtonSelected == buttonNo then\n onButtonUp(buttonNo)\n onClick(buttonNo)\nend\nMapScreenButtonSelected = -buttonNo","filter":{"args":[{"variable":"*"},{"variable":"*"}],"signature":"mouseUp(x,y)","slotKey":"0"},"key":"0"},{"code":"MapScreenMouseX = x\nMapScreenMouseY = y\nMapScreenMouseDown = true\nMapScreenButtonSelected = evaluateButtons()\nonButtonDown(MapScreenButtonSelected)\n","filter":{"args":[{"variable":"*"},{"variable":"*"}],"signature":"mouseDown(x,y)","slotKey":"0"},"key":"1"},{"code":"function Atlas()\n return {\n [0] = {\n [1]={\n GM=6930729684,\n bodyId=1,\n center={x=17465536.000,y=22665536.000,z=-34464.000},\n name='Madis',\n planetarySystemId=0,\n radius=44300\n },\n [2]={\n GM=157470826617,\n bodyId=2,\n center={x=-8.000,y=-8.000,z=-126303.000},\n name='Alioth',\n planetarySystemId=0,\n radius=126068\n },\n [3]={\n GM=11776905000,\n bodyId=3,\n center={x=29165536.000,y=10865536.000,z=65536.000},\n name='Thades',\n planetarySystemId=0,\n radius=49000\n },\n [4]={\n GM=14893847582,\n bodyId=4,\n center={x=-13234464.000,y=55765536.000,z=465536.000},\n name='Talemai',\n planetarySystemId=0,\n radius=57450\n },\n [5]={\n GM=16951680000,\n bodyId=5,\n center={x=-43534464.000,y=22565536.000,z=-48934464.000},\n name='Feli',\n planetarySystemId=0,\n radius=60000\n },\n [6]={\n GM=10502547741,\n bodyId=6,\n center={x=52765536.000,y=27165538.000,z=52065535.000},\n name='Sicari',\n planetarySystemId=0,\n radius=51100\n },\n [7]={\n GM=13033380591,\n bodyId=7,\n center={x=58665538.000,y=29665535.000,z=58165535.000},\n name='Sinnen',\n planetarySystemId=0,\n radius=54950\n },\n [8]={\n GM=18477723600,\n bodyId=8,\n center={x=80865538.000,y=54665536.000,z=-934463.940},\n name='Teoma',\n planetarySystemId=0,\n radius=62000\n },\n [9]={\n GM=18606274330,\n bodyId=9,\n center={x=-94134462.000,y=12765534.000,z=-3634464.000},\n name='Jago',\n planetarySystemId=0,\n radius=61590\n },\n [10]={\n GM=78480000,\n bodyId=10,\n center={x=17448118.224,y=22966846.286,z=143078.820},\n name='Madis Moon 1',\n planetarySystemId=0,\n radius=10000\n },\n [11]={\n GM=237402000,\n bodyId=11,\n center={x=17194626.000,y=22243633.880,z=-214962.810},\n name='Madis Moon 2',\n planetarySystemId=0,\n radius=11000\n },\n [12]={\n GM=265046609,\n bodyId=12,\n center={x=17520614.000,y=22184730.000,z=-309989.990},\n name='Madis Moon 3',\n planetarySystemId=0,\n radius=15005\n },\n [21]={\n GM=2118960000,\n bodyId=21,\n center={x=457933.000,y=-1509011.000,z=115524.000},\n name='Alioth Moon 1',\n planetarySystemId=0,\n radius=30000\n },\n [22]={\n GM=2165833514,\n bodyId=22,\n center={x=-1692694.000,y=729681.000,z=-411464.000},\n name='Alioth Moon 4',\n planetarySystemId=0,\n radius=30330\n },\n [26]={\n GM=68234043600,\n bodyId=26,\n center={x=-1404835.000,y=562655.000,z=-285074.000},\n name='Sanctuary',\n planetarySystemId=0,\n radius=83400\n },\n [30]={\n GM=211564034,\n bodyId=30,\n center={x=29214402.000,y=10907080.695,z=433858.200},\n name='Thades Moon 1',\n planetarySystemId=0,\n radius=14002\n },\n [31]={\n GM=264870000,\n bodyId=31,\n center={x=29404193.000,y=10432768.000,z=19554.131},\n name='Thades Moon 2',\n planetarySystemId=0,\n radius=15000\n },\n [40]={\n GM=141264000,\n bodyId=40,\n center={x=-13503090.000,y=55594325.000,z=769838.640},\n name='Talemai Moon 2',\n planetarySystemId=0,\n radius=12000\n },\n [41]={\n GM=106830900,\n bodyId=41,\n center={x=-12800515.000,y=55700259.000,z=325207.840},\n name='Talemai Moon 3',\n planetarySystemId=0,\n radius=11000\n },\n [42]={\n GM=264870000,\n bodyId=42,\n center={x=-13058408.000,y=55781856.000,z=740177.760},\n name='Talemai Moon 1',\n planetarySystemId=0,\n radius=15000\n },\n [50]={\n GM=499917600,\n bodyId=50,\n center={x=-43902841.780,y=22261034.700,z=-48862386.000},\n name='Feli Moon 1',\n planetarySystemId=0,\n radius=14000\n },\n [70]={\n GM=396912600,\n bodyId=70,\n center={x=58969616.000,y=29797945.000,z=57969449.000},\n name='Sinnen Moon 1',\n planetarySystemId=0,\n radius=17000\n },\n [100]={\n GM=13975172474,\n bodyId=100,\n center={x=98865536.000,y=-13534464.000,z=-934461.990},\n name='Lacobus',\n planetarySystemId=0,\n radius=55650\n },\n [101]={\n GM=264870000,\n bodyId=101,\n center={x=98905288.170,y=-13950921.100,z=-647589.530},\n name='Lacobus Moon 3',\n planetarySystemId=0,\n radius=15000\n },\n [102]={\n GM=444981600,\n bodyId=102,\n center={x=99180968.000,y=-13783862.000,z=-926156.400},\n name='Lacobus Moon 1',\n planetarySystemId=0,\n radius=18000\n },\n [103]={\n GM=211503600,\n bodyId=103,\n center={x=99250052.000,y=-13629215.000,z=-1059341.400},\n name='Lacobus Moon 2',\n planetarySystemId=0,\n radius=14000\n },\n [110]={\n GM=9204742375,\n bodyId=110,\n center={x=14165536.000,y=-85634465.000,z=-934464.300},\n name='Symeon',\n planetarySystemId=0,\n radius=49050\n },\n [120]={\n GM=7135606629,\n bodyId=120,\n center={x=2865536.700,y=-99034464.000,z=-934462.020},\n name='Ion',\n planetarySystemId=0,\n radius=44950\n },\n [121]={\n GM=106830900,\n bodyId=121,\n center={x=2472916.800,y=-99133747.000,z=-1133582.800},\n name='Ion Moon 1',\n planetarySystemId=0,\n radius=11000\n },\n [122]={\n GM=176580000,\n bodyId=122,\n center={x=2995424.500,y=-99275010.000,z=-1378480.700},\n name='Ion Moon 2',\n planetarySystemId=0,\n radius=15000\n }\n }\n }\n end\nfunction PlanetRef()\n--[[\n Provide coordinate transforms and access to kinematic related parameters\n Author: JayleBreak\n Usage (unit.start):\n PlanetaryReference = require('planetref')\n galaxyReference = PlanetaryReference(referenceTableSource)\n helios = galaxyReference[0] -- PlanetaryReference.PlanetarySystem instance\n alioth = helios[2] -- PlanetaryReference.BodyParameters instance\n Methods:\n PlanetaryReference:getPlanetarySystem - based on planetary system ID.\n PlanetaryReference.isMapPosition - 'true' if an instance of 'MapPosition'\n PlanetaryReference.createBodyParameters - for entry into reference table\n PlanetaryReference.BodyParameters - a class containing a body's information.\n PlanetaryReference.MapPosition - a class for map coordinates\n PlanetaryReference.PlanetarySystem - a container for planetary system info.\n PlanetarySystem:castIntersections - from a position in a given direction.\n PlanetarySystem:closestBody - to the specified coordinates.\n PlanetarySystem:convertToBodyIdAndWorldCoordinates - from map coordinates.\n PlanetarySystem:getBodyParameters - from reference table.\n PlanetarySystem:getPlanetarySystemId - for the instance.\n BodyParameters:convertToWorldCoordinates - from map coordinates\n BodyParameters:convertToMapPosition - from world coordinates\n BodyParameters:getAltitude - of world coordinates\n BodyParameters:getDistance - from center to world coordinates\n BodyParameters:getGravity - at a given position in world coordinates.\n Description\n An instance of the 'PlanetaryReference' \"class\" can contain transform and\n kinematic reference information for all planetary systems in DualUniverse.\n Each planetary system is identified by a numeric identifier. Currently,\n the only planetary system, Helios, has the identifier: zero. This \"class\"\n supports the indexing ('[]') operation which is equivalent to the\n use of the 'getPlanetarySystem' method. It also supports the 'pairs()'\n method for iterating over planetary systems.\n\n An instance of the 'PlanetarySystem' \"class\" contains all reference\n information for a specific system. It supports the indexing ('[]') and\n 'pairs()' functions which allows iteration over each \"body\" in the\n system where the key is the numeric body ID. It also supports the\n 'tostring()' method.\n An instance of the 'BodyParameters' \"class\" contains all reference\n information for a single celestial \"body\" (a moon or planet). It supports\n the 'tostring()' method, and contains the data members:\n planetarySystemId - numeric planetary system ID\n bodyId - numeric body ID\n radius - radius of the body in meters (zero altitude)\n center - world coordinates of the body's center position\n GM - the gravitation parameter (g = GM/radius^2)\n Note that the user is allowed to add custom fields (e.g. body name), but\n should insure that complex table values have the '__tostring' metamethod\n implemented.\n Transform and Kinematics:\n \"World\" coordinates is a cartesian coordinate system with an origin at an\n arbitrary fixed point in a planetary system and with distances measured in\n meters. The coordinates are expressible either as a simple table of 3 values\n or an instance of the 'vec3' class. In either case, the planetary system\n identity is implicit.\n \"Map\" coordinates is a geographic coordinate system with an origin at the\n center of an identified (by a numeric value) celestial body which is a\n member of an identified (also a numeric value) planetary system. Note that\n the convention that latitude, longitude, and altitude values will be the\n position's x, y, and z world coordinates in the special case of body ID 0.\n The kinematic parameters in the reference data permit calculations of the\n gravitational attraction of the celestial body on other objects.\n Reference Data:\n This is an example of reference data with a single entry assigned to\n planetary system ID 0, and body ID 2 ('Alioth'):\n referenceTable = {\n [0] = { [2] = { planetarySystemId = 0,\n bodyId = 2,\n radius = 126068,\n center = vec3({x=-8, y=-8, z=-126303}),\n GM = 1.572199+11 } -- as in F=-GMm/r^2\n }\n }\n ref=PlanetaryReference(referenceTable)\n Collecting Reference Data:\n A combination of information from the \"Map\" screen in the DU user interface,\n and values reported by the DU Lua API can be the source of the reference\n table's data (planetarySystemId, bodyId, and surfaceArea is from the user\n interface):\n referenceTable = {}\n referenceTable[planetarySystemId][bodyId] =\n PlanetaryReference.createBodyParameters(planetarySystemId,\n bodyId,\n surfaceArea,\n core.getConstructWorldPos(),\n core.getWorldVertical(),\n core.getAltitude(),\n core.g())\n Adapting Data Sources:\n Other sources of data can be adapted or converted. An example of adapting a\n table, defined in the file: 'planets.lua', containing information on a single\n planetary system and using celestial body name as the key follows (note that\n a 'name' field is added to the BodyParameters instance transparently after\n construction, and the '__pairs' meta function is required to support the\n 'closestBody' and '__tostring' methods):\n ref=PlanetaryReference(\n {[0] = setmetatable(require('planets'),\n { __index = function(bodies, bodyId)\n for _,v in pairs(bodies) do\n if v and v.bodyId == bodyId then return v end\n end\n return nil\n end,\n __pairs = function(bodies)\n return function(t, k)\n local nk, nv = next(t, k)\n if nv then\n local GM = nv.gravity * nv.radius^2\n local bp = BodyParameters(0,\n nv.id,\n nv.radius,\n nv.pos,\n GM)\n bp.name = nk\n return nk, bp\n end\n return nk, nv\n end, bodies, nil\n end })\n })\n\n Converting Data Sources:\n An instance of 'PlanetaryReference' that has been adapted to a data source\n can be used to convert that source to simple table. For example,\n using the adapted instance shown above:\n load('convertedData=' .. tostring(ref))()\n newRef=PlanetaryReference(convertedData)\n Also See: kepler.lua\n ]]--\n--[[ START OF LOCAL IMPLEMENTATION DETAILS ]]--\n-- Type checks\nlocal function isNumber(n) return type(n) == 'number' end\nlocal function isSNumber(n) return type(tonumber(n)) == 'number' end\nlocal function isTable(t) return type(t) == 'table' end\nlocal function isString(s) return type(s) == 'string' end\nlocal function isVector(v) return isTable(v)\n and isNumber(v.x and v.y and v.z) end\nlocal function isMapPosition(m) return isTable(m) and isNumber(m.latitude and\n m.longitude and\n m.altitude and\n m.bodyId and\n m.systemId) end\n-- Constants\nlocal deg2rad = math.pi/180\nlocal rad2deg = 180/math.pi\nlocal epsilon = 1e-10\nlocal num = ' *([+-]?%d+%.?%d*e?[+-]?%d*)'\nlocal posPattern = '::pos{' .. num .. ',' .. num .. ',' .. num .. ',' ..\n num .. ',' .. num .. '}'\n-- Utilities\nlocal utils = require('cpml.utils')\nlocal vec3 = require('cpml.vec3')\nlocal clamp = utils.clamp\nlocal function float_eq(a,b)\n if a == 0 then return math.abs(b) < 1e-09 end\n if b == 0 then return math.abs(a) < 1e-09 end\n return math.abs(a - b) < math.max(math.abs(a),math.abs(b))*epsilon\nend\nlocal function formatNumber(n)\n local result = string.gsub(\n string.reverse(string.format('%.4f',n)),\n '^0*%.?','')\n return result == '' and '0' or string.reverse(result)\nend\nlocal function formatValue(obj)\n if isVector(obj) then\n return string.format('{x=%.3f,y=%.3f,z=%.3f}', obj.x, obj.y, obj.z)\n end\n if isTable(obj) and not getmetatable(obj) then\n local list = {}\n local nxt = next(obj)\n if type(nxt) == 'nil' or nxt == 1 then -- assume this is an array\n list = obj\n else\n for k,v in pairs(obj) do\n local value = formatValue(v)\n if type(k) == 'number' then\n table.insert(list, string.format('[%s]=%s', k, value))\n else\n table.insert(list, string.format('%s=%s', k, value))\n end\n end\n end\n return string.format('{%s}', table.concat(list, ','))\n end\n if isString(obj) then\n return string.format(\"'%s'\", obj:gsub(\"'\",[[\\']]))\n end\n return tostring(obj)\nend\n-- CLASSES\n-- BodyParameters: Attributes of planetary bodies (planets and moons)\nlocal BodyParameters = {}\nBodyParameters.__index = BodyParameters\nBodyParameters.__tostring =\n function(obj, indent)\n local sep = indent or ''\n local keys = {}\n for k in pairs(obj) do table.insert(keys, k) end\n table.sort(keys)\n local list = {}\n for _, k in ipairs(keys) do\n local value = formatValue(obj[k])\n if type(k) == 'number' then\n table.insert(list, string.format('[%s]=%s', k, value))\n else\n table.insert(list, string.format('%s=%s', k, value))\n end\n end\n if indent then\n return string.format('%s%s',\n indent,\n table.concat(list, ',\\n' .. indent))\n end\n return string.format('{%s}', table.concat(list, ','))\n end\nBodyParameters.__eq = function(lhs, rhs)\n return lhs.planetarySystemId == rhs.planetarySystemId and\n lhs.bodyId == rhs.bodyId and\n float_eq(lhs.radius, rhs.radius) and\n float_eq(lhs.center.x, rhs.center.x) and\n float_eq(lhs.center.y, rhs.center.y) and\n float_eq(lhs.center.z, rhs.center.z) and\n float_eq(lhs.GM, rhs.GM)\n end\nlocal function mkBodyParameters(systemId, bodyId, radius, worldCoordinates, GM)\n -- 'worldCoordinates' can be either table or vec3\n assert(isSNumber(systemId),\n 'Argument 1 (planetarySystemId) must be a number:' .. type(systemId))\n assert(isSNumber(bodyId),\n 'Argument 2 (bodyId) must be a number:' .. type(bodyId))\n assert(isSNumber(radius),\n 'Argument 3 (radius) must be a number:' .. type(radius))\n assert(isTable(worldCoordinates),\n 'Argument 4 (worldCoordinates) must be a array or vec3.' ..\n type(worldCoordinates))\n assert(isSNumber(GM),\n 'Argument 5 (GM) must be a number:' .. type(GM))\n return setmetatable({planetarySystemId = tonumber(systemId),\n bodyId = tonumber(bodyId),\n radius = tonumber(radius),\n center = vec3(worldCoordinates),\n GM = tonumber(GM) }, BodyParameters)\nend\n-- MapPosition: Geographical coordinates of a point on a planetary body.\nlocal MapPosition = {}\nMapPosition.__index = MapPosition\nMapPosition.__tostring = function(p)\n return string.format('::pos{%d,%d,%s,%s,%s}',\n p.systemId,\n p.bodyId,\n formatNumber(p.latitude*rad2deg),\n formatNumber(p.longitude*rad2deg),\n formatNumber(p.altitude))\n end\nMapPosition.__eq = function(lhs, rhs)\n return lhs.bodyId == rhs.bodyId and\n lhs.systemId == rhs.systemId and\n float_eq(lhs.latitude, rhs.latitude) and\n float_eq(lhs.altitude, rhs.altitude) and\n (float_eq(lhs.longitude, rhs.longitude) or\n float_eq(lhs.latitude, math.pi/2) or\n float_eq(lhs.latitude, -math.pi/2))\n end\n-- latitude and longitude are in degrees while altitude is in meters\nlocal function mkMapPosition(overload, bodyId, latitude, longitude, altitude)\n local systemId = overload -- Id or '::pos{...}' string\n if isString(overload) and not longitude and not altitude and\n not bodyId and not latitude then\n systemId, bodyId, latitude, longitude, altitude =\n string.match(overload, posPattern)\n assert(systemId, 'Argument 1 (position string) is malformed.')\n else\n assert(isSNumber(systemId),\n 'Argument 1 (systemId) must be a number:' .. type(systemId))\n assert(isSNumber(bodyId),\n 'Argument 2 (bodyId) must be a number:' .. type(bodyId))\n assert(isSNumber(latitude),\n 'Argument 3 (latitude) must be in degrees:' .. type(latitude))\n assert(isSNumber(longitude),\n 'Argument 4 (longitude) must be in degrees:' .. type(longitude))\n assert(isSNumber(altitude),\n 'Argument 5 (altitude) must be in meters:' .. type(altitude))\n end\n systemId = tonumber(systemId)\n bodyId = tonumber(bodyId)\n latitude = tonumber(latitude)\n longitude = tonumber(longitude)\n altitude = tonumber(altitude)\n if bodyId == 0 then -- this is a hack to represent points in space\n return setmetatable({latitude = latitude,\n longitude = longitude,\n altitude = altitude,\n bodyId = bodyId,\n systemId = systemId}, MapPosition)\n end\n return setmetatable({latitude = deg2rad*clamp(latitude, -90, 90),\n longitude = deg2rad*(longitude % 360),\n altitude = altitude,\n bodyId = bodyId,\n systemId = systemId}, MapPosition)\nend\n-- PlanetarySystem - map body IDs to BodyParameters\nlocal PlanetarySystem = {}\nPlanetarySystem.__index = PlanetarySystem\nPlanetarySystem.__tostring =\n function (obj, indent)\n local sep = indent and (indent .. ' ' )\n local bdylist = {}\n local keys = {}\n for k in pairs(obj) do table.insert(keys, k) end\n table.sort(keys)\n for _, bi in ipairs(keys) do\n bdy = obj[bi]\n local bdys = BodyParameters.__tostring(bdy, sep)\n if indent then\n table.insert(bdylist,\n string.format('[%s]={\\n%s\\n%s}',\n bi, bdys, indent))\n else\n table.insert(bdylist, string.format(' [%s]=%s', bi, bdys))\n end\n end\n if indent then\n return string.format('\\n%s%s%s',\n indent,\n table.concat(bdylist, ',\\n' .. indent),\n indent)\n end\n return string.format('{\\n%s\\n}', table.concat(bdylist, ',\\n'))\n end\nlocal function mkPlanetarySystem(referenceTable)\n local atlas = {}\n local pid\n for _, v in pairs(referenceTable) do\n local id = v.planetarySystemId\n if type(id) ~= 'number' then\n error('Invalid planetary system ID: ' .. tostring(id))\n elseif pid and id ~= pid then\n error('Mismatch planetary system IDs: ' .. id .. ' and '\n .. pid)\n end\n local bid = v.bodyId\n if type(bid) ~= 'number' then\n error('Invalid body ID: ' .. tostring(bid))\n elseif atlas[bid] then\n error('Duplicate body ID: ' .. tostring(bid))\n end\n setmetatable(v.center, getmetatable(vec3.unit_x))\n atlas[bid] = setmetatable(v, BodyParameters)\n pid = id\n end\n return setmetatable(atlas, PlanetarySystem)\nend\n-- PlanetaryReference - map planetary system ID to PlanetarySystem\nPlanetaryReference = {}\nlocal function mkPlanetaryReference(referenceTable)\n return setmetatable({ galaxyAtlas = referenceTable or {} },\n PlanetaryReference)\nend\nPlanetaryReference.__index =\n function(t,i)\n if type(i) == 'number' then\n local system = t.galaxyAtlas[i]\n return mkPlanetarySystem(system)\n end\n return rawget(PlanetaryReference, i)\n end\nPlanetaryReference.__pairs =\n function(obj)\n return function(t, k)\n local nk, nv = next(t, k)\n return nk, nv and mkPlanetarySystem(nv)\n end, obj.galaxyAtlas, nil\n end\nPlanetaryReference.__tostring =\n function (obj)\n local pslist = {}\n for _,ps in pairs(obj or {}) do\n local psi = ps:getPlanetarySystemId()\n local pss = PlanetarySystem.__tostring(ps, ' ')\n table.insert(pslist,\n string.format(' [%s]={%s\\n }', psi, pss))\n end\n return string.format('{\\n%s\\n}\\n', table.concat(pslist,',\\n'))\n end\n--[[ START OF PUBLIC INTERFACE ]]--\n-- PlanetaryReference CLASS METHODS:\n--\n-- BodyParameters - create an instance of BodyParameters class\n-- planetarySystemId [in]: the body's planetary system ID.\n-- bodyId [in]: the body's ID.\n-- radius [in]: the radius in meters of the planetary body.\n-- bodyCenter [in]: the world coordinates of the center (vec3 or table).\n-- GM [in]: the body's standard gravitational parameter.\n-- return: an instance of BodyParameters class.\n--\nPlanetaryReference.BodyParameters = mkBodyParameters\n--\n-- MapPosition - create an instance of the MapPosition class\n-- overload [in]: either a planetary system ID or a position string ('::pos...')\n-- bodyId [in]: (ignored if overload is a position string) the body's ID.\n-- latitude [in]: (ignored if overload is a position string) the latitude.\n-- longitude [in]:(ignored if overload is a position string) the longitude.\n-- altitude [in]: (ignored if overload is a position string) the altitude.\n-- return: the class instance\n--\nPlanetaryReference.MapPosition = mkMapPosition\n--\n-- PlanetarySystem - create an instance of PlanetarySystem class\n-- referenceData [in]: a table (indexed by bodyId) of body reference info.\n-- return: the class instance\n--\nPlanetaryReference.PlanetarySystem = mkPlanetarySystem\n--\n-- createBodyParameters - create an instance of BodyParameters class\n-- planetarySystemId [in]: the body's planetary system ID.\n-- bodyId [in]: the body's ID.\n-- surfaceArea [in]: the body's surface area in square meters.\n-- aPosition [in]: world coordinates of a position near the body.\n-- verticalAtPosition [in]: a vector pointing towards the body center.\n-- altitudeAtPosition [in]: the altitude in meters at the position.\n-- gravityAtPosition [in]: the magnitude of the gravitational acceleration.\n-- return: an instance of BodyParameters class.\n--\nfunction PlanetaryReference.createBodyParameters(planetarySystemId,\n bodyId,\n surfaceArea,\n aPosition,\n verticalAtPosition,\n altitudeAtPosition,\n gravityAtPosition)\n assert(isSNumber(planetarySystemId),\n 'Argument 1 (planetarySystemId) must be a number:' ..\n type(planetarySystemId))\n assert(isSNumber(bodyId),\n 'Argument 2 (bodyId) must be a number:' .. type(bodyId))\n assert(isSNumber(surfaceArea),\n 'Argument 3 (surfaceArea) must be a number:' .. type(surfaceArea))\n assert(isTable(aPosition),\n 'Argument 4 (aPosition) must be an array or vec3:' ..\n type(aPosition))\n assert(isTable(verticalAtPosition),\n 'Argument 5 (verticalAtPosition) must be an array or vec3:' ..\n type(verticalAtPosition))\n assert(isSNumber(altitudeAtPosition),\n 'Argument 6 (altitude) must be in meters:' ..\n type(altitudeAtPosition))\n assert(isSNumber(gravityAtPosition),\n 'Argument 7 (gravityAtPosition) must be number:' ..\n type(gravityAtPosition))\n local radius = math.sqrt(surfaceArea/4/math.pi)\n local distance = radius + altitudeAtPosition\n local center = vec3(aPosition) + distance*vec3(verticalAtPosition)\n local GM = gravityAtPosition * distance * distance\n return mkBodyParameters(planetarySystemId, bodyId, radius, center, GM)\nend\n--\n-- isMapPosition - check for the presence of the 'MapPosition' fields\n-- valueToTest [in]: the value to be checked\n-- return: 'true' if all required fields are present in the input value\n--\nPlanetaryReference.isMapPosition = isMapPosition\n-- PlanetaryReference INSTANCE METHODS:\n--\n-- getPlanetarySystem - get the planetary system using ID or MapPosition as key\n-- overload [in]: either the planetary system ID or a MapPosition that has it.\n-- return: instance of 'PlanetarySystem' class or nil on error\n--\nfunction PlanetaryReference:getPlanetarySystem(overload)\n --if galaxyAtlas then\n local planetarySystemId = overload\n if isMapPosition(overload) then\n planetarySystemId = overload.systemId\n end\n if type(planetarySystemId) == 'number' then\n local system = self.galaxyAtlas[i]\n if system then\n if getmetatable(nv) ~= PlanetarySystem then\n system = mkPlanetarySystem(system)\n end\n return system\n end\n end\n --end\n --return nil\nend\n-- PlanetarySystem INSTANCE METHODS:\n--\n-- castIntersections - Find the closest body that intersects a \"ray cast\".\n-- origin [in]: the origin of the \"ray cast\" in world coordinates\n-- direction [in]: the direction of the \"ray cast\" as a 'vec3' instance.\n-- sizeCalculator [in]: (default: returns 1.05*radius) Returns size given body.\n-- bodyIds[in]: (default: all IDs in system) check only the given IDs.\n-- return: The closest body that blocks the cast or 'nil' if none.\n--\nfunction PlanetarySystem:castIntersections(origin,\n direction,\n sizeCalculator,\n bodyIds)\n local sizeCalculator = sizeCalculator or\n function (body) return 1.05*body.radius end\n local candidates = {}\n if bodyIds then\n for _,i in ipairs(bodyIds) do candidates[i] = self[i] end\n else\n bodyIds = {}\n for k,body in pairs(self) do\n table.insert(bodyIds, k)\n candidates[k] = body\n end\n end\n local function compare(b1,b2)\n local v1 = candidates[b1].center - origin\n local v2 = candidates[b2].center - origin\n return v1:len() < v2:len()\n end\n table.sort(bodyIds, compare)\n local dir = direction:normalize()\n for i, id in ipairs(bodyIds) do\n local body = candidates[id]\n local c_oV3 = body.center - origin\n local radius = sizeCalculator(body)\n local dot = c_oV3:dot(dir)\n local desc = dot^2 - (c_oV3:len2() - radius^2)\n if desc >= 0 then\n local root = math.sqrt(desc)\n local farSide = dot + root\n local nearSide = dot - root\n if nearSide > 0 then\n return body, farSide, nearSide\n elseif farSide > 0 then\n return body, farSide, nil\n end\n end\n end\n return nil, nil, nil\nend\n--\n-- closestBody - find the closest body to a given set of world coordinates\n-- coordinates [in]: the world coordinates of position in space\n-- return: an instance of the BodyParameters object closest to 'coordinates'\n--\nfunction PlanetarySystem:closestBody(coordinates)\n assert(type(coordinates) == 'table', 'Invalid coordinates.')\n local minDistance2, body\n local coord = vec3(coordinates)\n for _,params in pairs(self) do\n local distance2 = (params.center - coord):len2()\n if not body or distance2 < minDistance2 then\n body = params\n minDistance2 = distance2\n end\n end\n return body\nend\n--\n-- convertToBodyIdAndWorldCoordinates - map to body Id and world coordinates\n-- overload [in]: an instance of MapPosition or a position string ('::pos...)\n-- return: a vec3 instance containing the world coordinates or 'nil' on error.\n--\nfunction PlanetarySystem:convertToBodyIdAndWorldCoordinates(overload)\n local mapPosition = overload\n if isString(overload) then\n mapPosition = mkMapPosition(overload)\n end\n if mapPosition.bodyId == 0 then\n return 0, vec3(mapPosition.latitude,\n mapPosition.longitude,\n mapPosition.altitude)\n end\n local params = self:getBodyParameters(mapPosition)\n if params then\n return mapPosition.bodyId,\n params:convertToWorldCoordinates(mapPosition)\n end\nend\n--\n-- getBodyParameters - get or create an instance of BodyParameters class\n-- overload [in]: either an instance of MapPosition or a body's ID.\n-- return: a BodyParameters instance or 'nil' if body ID is not found.\n--\nfunction PlanetarySystem:getBodyParameters(overload)\n local bodyId = overload\n if isMapPosition(overload) then\n bodyId = overload.bodyId\n end\n assert(isSNumber(bodyId),\n 'Argument 1 (bodyId) must be a number:' .. type(bodyId))\n return self[bodyId]\nend\n--\n-- getPlanetarySystemId - get the planetary system ID for this instance\n-- return: the planetary system ID or nil if no planets are in the system.\n--\nfunction PlanetarySystem:getPlanetarySystemId()\n local k, v = next(self)\n return v and v.planetarySystemId\nend\n-- BodyParameters INSTANCE METHODS:\n--\n-- convertToMapPosition - create an instance of MapPosition from coordinates\n-- worldCoordinates [in]: the world coordinates of the map position.\n-- return: an instance of MapPosition class\n--\nfunction BodyParameters:convertToMapPosition(worldCoordinates)\n assert(isTable(worldCoordinates),\n 'Argument 1 (worldCoordinates) must be an array or vec3:' ..\n type(worldCoordinates))\n local worldVec = vec3(worldCoordinates)\n if self.bodyId == 0 then\n return setmetatable({latitude = worldVec.x,\n longitude = worldVec.y,\n altitude = worldVec.z,\n bodyId = 0,\n systemId = self.planetarySystemId}, MapPosition)\n end\n local coords = worldVec - self.center\n local distance = coords:len()\n local altitude = distance - self.radius\n local latitude = 0\n local longitude = 0\n if not float_eq(distance, 0) then\n local phi = math.atan(coords.y, coords.x)\n longitude = phi >= 0 and phi or (2*math.pi + phi)\n latitude = math.pi/2 - math.acos(coords.z/distance)\n end\n return setmetatable({latitude = latitude,\n longitude = longitude,\n altitude = altitude,\n bodyId = self.bodyId,\n systemId = self.planetarySystemId}, MapPosition)\nend\n--\n-- convertToWorldCoordinates - convert a map position to world coordinates\n-- overload [in]: an instance of MapPosition or a position string ('::pos...')\n--\nfunction BodyParameters:convertToWorldCoordinates(overload)\n local mapPosition = isString(overload) and\n mkMapPosition(overload) or overload\n if mapPosition.bodyId == 0 then -- support deep space map position\n return vec3(mapPosition.latitude,\n mapPosition.longitude,\n mapPosition.altitude)\n end\n assert(isMapPosition(mapPosition),\n 'Argument 1 (mapPosition) is not an instance of \"MapPosition\".')\n assert(mapPosition.systemId == self.planetarySystemId,\n 'Argument 1 (mapPosition) has a different planetary system ID.')\n assert(mapPosition.bodyId == self.bodyId,\n 'Argument 1 (mapPosition) has a different planetary body ID.')\n local xproj = math.cos(mapPosition.latitude)\n return self.center + (self.radius + mapPosition.altitude) *\n vec3(xproj*math.cos(mapPosition.longitude),\n xproj*math.sin(mapPosition.longitude),\n math.sin(mapPosition.latitude))\nend\n--\n-- getAltitude - calculate the altitude of a point given in world coordinates.\n-- worldCoordinates [in]: the world coordinates of the point.\n-- return: the altitude in meters\n--\nfunction BodyParameters:getAltitude(worldCoordinates)\n return (vec3(worldCoordinates) - self.center):len() - self.radius\nend\n--\n-- getDistance - calculate the distance to a point given in world coordinates.\n-- worldCoordinates [in]: the world coordinates of the point.\n-- return: the distance in meters\n--\nfunction BodyParameters:getDistance(worldCoordinates)\n return (vec3(worldCoordinates) - self.center):len()\nend\n--\n-- getGravity - calculate the gravity vector induced by the body.\n-- worldCoordinates [in]: the world coordinates of the point.\n-- return: the gravity vector in meter/seconds^2\n--\nfunction BodyParameters:getGravity(worldCoordinates)\n local radial = self.center - vec3(worldCoordinates) -- directed towards body\n local len2 = radial:len2()\n return (self.GM/len2) * radial/math.sqrt(len2)\nend\n-- end of module\nreturn setmetatable(PlanetaryReference,\n { __call = function(_,...)\n return mkPlanetaryReference(...)\n end })\nend\nfunction Keplers()\n --[[\n Provides methods for computing orbital information for an object\n Usage:\n Kepler = require('autoconf.custom.kepler')\n alioth = Kepler({ GM=157470826617,\n bodyId=2,\n center={x=-8.000,y=-8.000,z=-126303.000},\n name='Alioth',\n planetarySystemId=0,\n radius=126068\n })\n altitude = 6000\n position = '::pos{0,2,0,0,6000}'\n e, o = alioth:escapeAndOrbitalSpeed(altitude)\n orbit = alioth:orbitalParameters(position, {0, o+1, 0})\n print(\"Eccentricity \" .. orbit.eccentricity)\n print(\"Perihelion \" .. orbit.periapsis.altitude)\n print(\"Max. speed \" .. orbit.periapsis.speed)\n print(\"Circular orbit speed \" .. orbit.periapsis.circularOrbitSpeed)\n print(\"Aphelion \" .. orbit.apoapsis.altitude)\n print(\"Min. speed \" .. orbit.apoapsis.speed)\n print(\"Orbital period \" .. orbit.period)\n --- output:\n Eccentricity 0.0018324307017878\n Perihelion 6000.0\n Max. speed 1092.9462297033\n Circular orbit speed 1091.9462297033\n Aphelion 6484.8994605062\n Min. speed 1088.9480596194\n Orbital period 762.02818214049\n Methods:\n Kepler:escapeAndOrbitalSpeed - for a given celestial body and altitude.\n Kepler:orbitalParameters - for a given massless object and a celestial body.\n Description\n The motion of an object in the vicinity of substantially larger mass is\n in the domain of the \"2-body problem\". By assuming the object whose motion\n is of interest is of negligable mass simplifies the calculations of:\n the speed to escape the body, the speed of a circular orbit, and the\n parameters defining the orbit of the object (or the lack of orbit as the\n case may be).\n Orbital Parameters:\n periapsis - the closest approach to the planet\n apoapsis - the furthest point from the planet if in orbit (otherwise nil)\n eccentricity - 0 for circular orbits\n <1 for elliptical orbits\n 1 for parabiolic trajectory\n >1 for hyperbolic trajectory\n period - time (in seconds) to complete an orbit\n Also See: planetref.lua\n]]--\nlocal vec3 = require('cpml.vec3')\nlocal PlanetRef = PlanetRef()\nlocal function isString(s) return type(s) == 'string' end\nlocal function isTable(t) return type(t) == 'table' end\nlocal function float_eq(a,b)\n if a == 0 then return math.abs(b) < 1e-09 end\n if b == 0 then return math.abs(a) < 1e-09 end\n return math.abs(a - b) < math.max(math.abs(a),math.abs(b))*epsilon\nend\nKepler = {}\nKepler.__index = Kepler\n--\n-- escapeAndOrbitalSpeed - speed required to escape and for a circular orbit\n-- altitude [in]: the height of the orbit in meters above \"sea-level\"\n-- return: the speed in m/s needed to escape the celestial body and to orbit it.\n--\nfunction Kepler:escapeAndOrbitalSpeed(altitude)\n assert(self.body)\n -- P = -GMm/r and KE = mv^2/2 (no lorentz factor used)\n -- mv^2/2 = GMm/r\n -- v^2 = 2GM/r\n -- v = sqrt(2GM/r1)\n local distance = altitude + self.body.radius\n if not float_eq(distance, 0) then\n local orbit = math.sqrt(self.body.GM/distance)\n return math.sqrt(2)*orbit, orbit\n end\n return nil, nil\nend\n--\n-- orbitalParameters: determine the orbital elements for a two-body system.\n-- overload [in]: the world coordinates or map coordinates of a massless object.\n-- velocity [in]: The velocity of the massless point object in m/s.\n-- return: the 6 orbital elements for the massless object.\n--\nfunction Kepler:orbitalParameters(overload, velocity)\n assert(self.body)\n assert(isTable(overload) or isString(overload))\n assert(isTable(velocity))\n local pos = (isString(overload) or PlanetRef.isMapPosition(overload)) and\n self.body:convertToWorldCoordinates(overload) or\n vec3(overload)\n local v = vec3(velocity)\n local r = pos - self.body.center\n local v2 = v:len2()\n local d = r:len()\n local mu = self.body.GM\n local e = ((v2 - mu/d)*r - r:dot(v)*v)/mu\n local a = mu/(2*mu/d - v2)\n local ecc = e:len()\n local dir = e:normalize()\n local pd = a*(1-ecc)\n local ad = a*(1+ecc)\n local per = pd*dir + self.body.center\n local apo = ecc <= 1 and -ad*dir + self.body.center or nil\n local trm = math.sqrt(a*mu*(1-ecc*ecc))\n local Period = apo and 2*math.pi*math.sqrt(a^3/mu)\n -- These are great and all, but, I need more.\n local trueAnomaly = math.acos((e:dot(r))/(ecc*d))\n if r:dot(v) < 0 then\n trueAnomaly = -(trueAnomaly - 2*math.pi)\n end\n -- Apparently... cos(EccentricAnomaly) = (cos(trueAnomaly) + eccentricity)/(1 + eccentricity * cos(trueAnomaly))\n local EccentricAnomaly = math.acos((math.cos(trueAnomaly) + ecc)/(1 + ecc * math.cos(trueAnomaly)))\n -- Then.... apparently if this is below 0, we should add 2pi to it\n -- I think also if it's below 0, we're past the apoapsis?\n local timeTau = EccentricAnomaly\n if timeTau < 0 then\n timeTau = timeTau + 2*math.pi\n end\n -- So... time since periapsis...\n -- Is apparently easy if you get mean anomly. t = M/n where n is mean motion, = 2*pi/Period\n\n\n local MeanAnomaly = timeTau - ecc * math.sin(timeTau)\n local TimeSincePeriapsis = MeanAnomaly/(2*math.pi/Period)\n --system.print(MeanAnomaly .. \" - \" .. TimeSincePeriapsis .. \" - \" .. Period .. \" - \" .. EccentricAnomaly .. \" - \" .. timeTau .. \" - \" .. trueAnomaly)\n -- Mean anom is 0 at periapsis, positive before it... and positive after it.\n -- I guess this is why I needed to use timeTau and not EccentricAnomaly here\n\n local TimeToPeriapsis = Period - TimeSincePeriapsis\n local TimeToApoapsis = TimeToPeriapsis + Period/2\n if trueAnomaly - math.pi > 0 then -- TBH I think something's wrong in my formulas because I needed this.\n TimeToPeriapsis = TimeSincePeriapsis\n TimeToApoapsis = TimeToPeriapsis + Period/2\n end\n if TimeToApoapsis > Period then\n TimeToApoapsis = TimeToApoapsis - Period\n end\n return { periapsis = { position = per,\n speed = trm/pd,\n circularOrbitSpeed = math.sqrt(mu/pd),\n altitude = pd - self.body.radius},\n apoapsis = apo and\n { position = apo,\n speed = trm/ad,\n circularOrbitSpeed = math.sqrt(mu/ad),\n altitude = ad - self.body.radius},\n currentVelocity = v,\n currentPosition = pos,\n eccentricity = ecc,\n period = Period,\n eccentricAnomaly = EccentricAnomaly,\n meanAnomaly = MeanAnomaly,\n timeToPeriapsis = TimeToPeriapsis,\n timeToApoapsis = TimeToApoapsis\n }\nend\n\nlocal function new(bodyParameters)\n local params = PlanetRef.BodyParameters(bodyParameters.planetarySystemId,\n bodyParameters.bodyId,\n bodyParameters.radius,\n bodyParameters.center,\n bodyParameters.GM)\n return setmetatable({body = params}, Kepler)\nend\nreturn setmetatable(Kepler, { __call = function(_,...) return new(...) end })\nend\nfunction Kinematics()\n --[[\n DualUniverse kinematic equations\n Author: JayleBreak\n Usage (unit.start):\n Kinematics = require('autoconf.custom.kinematics')\n Methods:\n computeAccelerationTime - \"relativistic\" version of t = (vf - vi)/a\n computeDistanceAndTime - Return distance & time needed to reach final speed.\n computeTravelTime - \"relativistic\" version of t=(sqrt(2ad+v^2)-v)/a\n Description\n DualUniverse increases the effective mass of constructs as their absolute\n speed increases by using the \"lorentz\" factor (from relativity) as the scale\n factor. This results in an upper bound on the absolute speed of constructs\n (excluding \"warp\" drive) that is set to 30 000 KPH (8 333 MPS). This module\n provides utilities for computing some physical quantities taking this\n scaling into account.\n]]--\nlocal Kinematic = {} -- just a namespace\nlocal C = 30000000/3600\nlocal C2 = C*C\nlocal ITERATIONS = 100 -- iterations over engine \"warm-up\" period\nlocal function lorentz(v) return 1/math.sqrt(1 - v*v/C2) end\n--\n-- computeAccelerationTime - \"relativistic\" version of t = (vf - vi)/a\n-- initial [in]: initial (positive) speed in meters per second.\n-- acceleration [in]: constant acceleration until 'finalSpeed' is reached.\n-- final [in]: the speed at the end of the time interval.\n-- return: the time in seconds spent in traversing the distance\n--\nfunction Kinematic.computeAccelerationTime(initial, acceleration, final)\n -- The low speed limit of following is: t=(vf-vi)/a (from: vf=vi+at)\n local k1 = C*math.asin(initial/C)\n return (C * math.asin(final/C) - k1)/acceleration\nend\n--\n-- computeDistanceAndTime - Return distance & time needed to reach final speed.\n-- initial[in]: Initial speed in meters per second.\n-- final[in]: Final speed in meters per second.\n-- restMass[in]: Mass of the construct at rest in Kg.\n-- thrust[in]: Engine's maximum thrust in Newtons.\n-- t50[in]: (default: 0) Time interval to reach 50% thrust in seconds.\n-- brakeThrust[in]: (default: 0) Constant thrust term when braking.\n-- return: Distance (in meters), time (in seconds) required for change.\n--\nfunction Kinematic.computeDistanceAndTime(initial,\n final,\n restMass,\n thrust,\n t50,\n brakeThrust)\n -- This function assumes that the applied thrust is colinear with the\n -- velocity. Furthermore, it does not take into account the influence\n -- of gravity, not just in terms of its impact on velocity, but also\n -- its impact on the orientation of thrust relative to velocity.\n -- These factors will introduce (usually) small errors which grow as\n -- the length of the trip increases.\n t50 = t50 or 0\n brakeThrust = brakeThrust or 0 -- usually zero when accelerating\n local tau0 = lorentz(initial)\n local speedUp = initial <= final\n local a0 = thrust * (speedUp and 1 or -1)/restMass\n local b0 = -brakeThrust/restMass\n local totA = a0+b0\n if speedUp and totA <= 0 or not speedUp and totA >= 0 then\n return -1, -1 -- no solution\n end\n local distanceToMax, timeToMax = 0, 0\n -- If, the T50 time is set, then assume engine is at zero thrust and will\n -- reach full thrust in 2*T50 seconds. Thrust curve is given by:\n -- Thrust: F(z)=(a0*(1+sin(z))+2*b0)/2 where z=pi*(t/t50 - 1)/2\n -- Acceleration is given by F(z)/m(z) where m(z) = m/sqrt(1-v^2/c^2)\n -- or v(z)' = (a0*(1+sin(z))+2*b0)*sqrt(1-v(z)^2/c^2)/2\n if a0 ~= 0 and t50 > 0 then\n -- Closed form solution for velocity exists:\n -- v(t) = -c*tan(w)/sqrt(tan(w)^2+1) => w = -asin(v/c)\n -- w=(pi*t*(a0/2+b0)-a0*t50*sin(pi*t/2/t50)+*pi*c*k1)/pi/c\n -- @ t=0, v(0) = vi\n -- pi*c*k1/pi/c = -asin(vi/c)\n -- k1 = asin(vi/c)\n local k1 = math.asin(initial/C)\n local c1 = math.pi*(a0/2+b0)\n local c2 = a0*t50\n local c3 = C*math.pi\n local v = function(t)\n local w = (c1*t - c2*math.sin(math.pi*t/2/t50) + c3*k1)/c3\n local tan = math.tan(w)\n return C*tan/math.sqrt(tan*tan+1)\n end\n local speedchk = speedUp and function(s) return s >= final end or\n function(s) return s <= final end\n timeToMax = 2*t50\n if speedchk(v(timeToMax)) then\n local lasttime = 0\n while math.abs(timeToMax - lasttime) > 0.5 do\n local t = (timeToMax + lasttime)/2\n if speedchk(v(t)) then\n timeToMax = t\n else\n lasttime = t\n end\n end\n end\n -- There is no closed form solution for distance in this case.\n -- Numerically integrate for time t=0 to t=2*T50 (or less)\n local lastv = initial\n local tinc = timeToMax/ITERATIONS\n for step = 1, ITERATIONS do\n local speed = v(step*tinc)\n distanceToMax = distanceToMax + (speed+lastv)*tinc/2\n lastv = speed\n end\n if timeToMax < 2*t50 then\n return distanceToMax, timeToMax\n end\n initial = lastv\n end\n -- At full thrust, acceleration only depends on the Lorentz factor:\n -- v(t)' = (F/m(v)) = a*sqrt(1-v(t)^2/c^2) where a = a0+b0\n -- -> v = c*sin((at+k1)/c)\n -- @ t=0, v=vi: k1 = c*asin(vi/c)\n -- -> t = (c*asin(v/c) - k1)/a\n -- x(t)' = c*sin((at+k1)/c)\n -- x = k2 - c^2 cos((at+k1)/c)/a\n -- @ t=0, x=0: k2 = c^2 * cos(k1/c)/a\n local k1 = C*math.asin(initial/C)\n local time = (C * math.asin(final/C) - k1)/totA\n local k2 = C2 *math.cos(k1/C)/totA\n local distance = k2 - C2 * math.cos((totA*time + k1)/C)/totA\n return distance+distanceToMax, time+timeToMax\nend\n--\n-- computeTravelTime - \"relativistic\" version of t=(sqrt(2ad+v^2)-v)/a\n-- initialSpeed [in]: initial (positive) speed in meters per second\n-- acceleration [in]: constant acceleration until 'distance' is traversed\n-- distance [in]: the distance traveled in meters\n-- return: the time in seconds spent in traversing the distance\n--\nfunction Kinematic.computeTravelTime(initial, acceleration, distance)\n -- The low speed limit of following is: t=(sqrt(2ad+v^2)-v)/a\n -- (from: d=vt+at^2/2)\n if distance == 0 then return 0 end\n if acceleration > 0 then\n local k1 = C*math.asin(initial/C)\n local k2 = C2*math.cos(k1/C)/acceleration\n return (C*math.acos(acceleration*(k2 - distance)/C2) - k1)/acceleration\n end\n assert(initial > 0, 'Acceleration and initial speed are both zero.')\n return distance/initial\nend\nfunction Kinematic.lorentz(v) return lorentz(v) end\nreturn Kinematic\nend\nPlanetaryReference = PlanetRef()\ngalaxyReference = PlanetaryReference(Atlas())\nKinematic = Kinematics()\nKep = Keplers()\nfunction getDistanceDisplayString(distance)\n local su = distance > 100000\n local result = \"\"\n if su then\n -- Convert to SU\n result = round(distance/1000/200,1) .. \" SU\"\n else\n -- Convert to KM\n result = round(distance/1000,1) .. \" KM\"\n end\n\n return result\nend\n\nPlanetaryReference = PlanetRef()\ngalaxyReference = PlanetaryReference(Atlas())\n\nMapScreenButtons = {}\nMapScreenMouseX = 0\nMapScreenMouseY = 0\nMapScreenMouseDown = false\nMapScreenButtonSelected = 0\nlocal worldPos = vec3(core.getConstructWorldPos())\nlocal locX = (worldPos.x/400000)\nlocal locY = (worldPos.y/400000)*(-1)\nlocal destX = 0\nlocal destY = 0\nlocal sudistance = 0\nlocal loc = vec3(core.getConstructWorldPos())\nlocal ion = galaxyReference[0][120] ---uses Atlas functions\nlocal thades = vec3(29165536.000, 10865536.000, 65536.000)\nlocal sinnen = vec3(58665536.000, 29665536.000, 58165536.000)\nlocal alioth = galaxyReference[0][2] ---uses Atlas functions\nlocal madis = vec3(17465536.000, 22665536.000, -34464.000)\nlocal jago = vec3(-94134464.000, 12765536.000, -3634464.000)\nlocal symeon = vec3(14165536.000, -85634464.000, -934464.000)\nlocal lacobus = vec3(98865536.000, -13534464.000, -934464.000)\nlocal teoma = vec3(80865536.000, 54665536.000, -934464.000)\nlocal feli = vec3(-43534464.000, 22565536.000, -48934464.000)\nlocal talemai = vec3(-13234464.000, 55765536.000, 465536.000)\nlocal sicari = vec3(52765536.000, 27165536.000, 52065536.000)\nlocal distion = math.floor(ion:getDistance(loc)/200000) ---uses getDistance functions----\nlocal distthades = string.format(\"%.2f\", math.sqrt((loc.x-thades.x)^2+(loc.y-thades.y)^2+(loc.z-thades.z)^2)/200000)\nlocal distalioth = math.floor(alioth:getDistance(loc)/200000) ---uses getDistance functions----\nlocal distmadis = string.format(\"%.2f\", math.sqrt((loc.x-madis.x)^2+(loc.y-madis.y)^2+(loc.z-madis.z)^2)/200000)\nlocal distjago = string.format(\"%.2f\", math.sqrt((loc.x-jago.x)^2+(loc.y-jago.y)^2+(loc.z-jago.z)^2)/200000)\nlocal distlacobus = string.format(\"%.2f\", math.sqrt((loc.x-lacobus.x)^2+(loc.y-lacobus.y)^2+(loc.z-lacobus.z)^2)/200000)\nlocal distteoma = string.format(\"%.2f\", math.sqrt((loc.x-teoma.x)^2+(loc.y-teoma.y)^2+(loc.z-teoma.z)^2)/200000)\nlocal distsymeon = string.format(\"%.2f\", math.sqrt((loc.x-symeon.x)^2+(loc.y-symeon.y)^2+(loc.z-symeon.z)^2)/200000)\nlocal distfeli = string.format(\"%.2f\", math.sqrt((loc.x-feli.x)^2+(loc.y-feli.y)^2+(loc.z-feli.z)^2)/200000)\nlocal distsinnen = string.format(\"%.2f\", math.sqrt((loc.x-sinnen.x)^2+(loc.y-sinnen.y)^2+(loc.z-sinnen.z)^2)/200000)\nlocal disttalemai = string.format(\"%.2f\", math.sqrt((loc.x-talemai.x)^2+(loc.y-talemai.y)^2+(loc.z-talemai.z)^2)/200000)\nlocal distsicari = string.format(\"%.2f\", math.sqrt((loc.x-sicari.x)^2+(loc.y-sicari.y)^2+(loc.z-sicari.z)^2)/200000)\nselection = 0\n\n\n for i = 1,1 do\n local button = {id = (\"b\"..1), enabled=true, td=\"<td>\", top=2/100, bottom=13/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 2,2 do\n local button = {id = (\"b\"..2), enabled=true, td=\"<td>\", top=15/100, bottom=26/100, left=1/100, right=30/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 3,3 do\n local button = {id = (\"b\"..3), enabled=true, td=\"<td>\", top=27/100, bottom=38/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 4,4 do\n local button = {id = (\"b\"..4), enabled=true, td=\"<td>\", top=39/100, bottom=50/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 5,5 do\n local button = {id = (\"b\"..5), enabled=true, td=\"<td>\", top=51/100, bottom=62/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 6,6 do\n local button = {id = (\"b\"..6), enabled=true, td=\"<td>\", top=64/100, bottom=75/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 7,7 do\n local button = {id = (\"b\"..7), enabled=true, td=\"<td>\", top=2/100, bottom=13/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 8,8 do\n local button = {id = (\"b\"..8), enabled=true, td=\"<td>\", top=15/100, bottom=26/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 9,9 do\n local button = {id = (\"b\"..9), enabled=true, td=\"<td>\", top=27/100, bottom=38/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 10,10 do\n local button = {id = (\"b\"..10), enabled=true, td=\"<td>\", top=39/100, bottom=50/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 11,11 do\n local button = {id = (\"b\"..11), enabled=true, td=\"<td>\", top=51/100, bottom=62/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 12,12 do\n local button = {id = (\"b\"..12), enabled=true, td=\"<td>\", top=64/100, bottom=75/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 13,13 do\n local button = {id = (\"b\"..13), enabled=true, td=\"<td>\", top=90/100, bottom=100/100, left=1/100, right=18/100}\n table.insert(MapScreenButtons, button)\nend\nfunction evaluateButtons()\n local selected = 0\n\n if #MapScreenButtons >= 1 then\n -- Set button styles\n for i, button in ipairs(MapScreenButtons) do\n if button.left < MapScreenMouseX and MapScreenMouseX < button.right and button.top < MapScreenMouseY and MapScreenMouseY < button.bottom then\n if MapScreenMouseDown and MapScreenButtonSelected == i then\n end\n selected = i\n end\n if not button.enabled then\n end\n\n end\n end\n return selected\nend\n\nfunction onButtonDown(buttonNo)\n local button = MapScreenButtons[buttonNo]\n if not button or not button.enabled then\n\treturn\n end\nend\nfunction onButtonUp(buttonNo)\n local button = MapScreenButtons[buttonNo]\n if not button or not button.enabled then\n return\n end\nfunction onClick(buttonNo)\n local button = MapScreenButtons[buttonNo]\n if not button or not button.enabled then\n return\n end\nend\n\n\n\n if buttonNo == 1 then\ndestX = 0\ndestY = 0\nselection = 1\nsudistance = distalioth\n elseif buttonNo == 2 then\ndestX = 43\ndestY = -56\nselection = 2\nsudistance = distmadis\n elseif buttonNo == 3 then\ndestX = 73\ndestY = -27\nselection = 3\nsudistance = distthades\n elseif buttonNo == 4 then\ndestX = -33\ndestY = -139\nselection = 4\nsudistance = disttalemai\n elseif buttonNo == 5 then\ndestX = -109\ndestY = -56\nselection = 5\nsudistance = distfeli\n elseif buttonNo == 6 then\ndestX = 131\ndestY = -68\nselection = 6\nsudistance = distsicari\n elseif buttonNo == 7 then\ndestX = 35\ndestY = 214\nselection = 7\nsudistance = distsymeon\n elseif buttonNo == 8 then\ndestX = 146\ndestY = -74\nselection = 8\nsudistance = distsinnen\n elseif buttonNo == 9 then\ndestX = -235\ndestY = -32\nselection = 9\nsudistance = distjago\n elseif buttonNo == 10 then\ndestX = 202\ndestY = -137\nselection = 10\nsudistance = distteoma\n elseif buttonNo == 11 then\ndestX = 7\ndestY = 247\nselection = 11\nsudistance = distion\n elseif buttonNo == 12 then\ndestX = 247\ndestY = 34\nselection = 12\nsudistance = distlacobus\n elseif buttonNo == 13 then\n unit.exit()\n end\nend\n\n\nlocal floor = math.floor\nlocal concat = table.concat\n\nlocal secondsInMinute = 60\nlocal secondsInHour = secondsInMinute * 60\nlocal secondsInDay = secondsInHour * 24\nlocal secondsInYear = 365.2419 * secondsInDay\n\nlocal minTotalSecondsToShowOnlyYears = secondsInYear * 10\n\n---@param totalSeconds number\n---@param maxComponents nil|number\nlocal function formatTimeWithUnits (totalSeconds, maxComponents)\n maxComponents = maxComponents or 2\n\n local buffer = {}\n\n if totalSeconds < 0 then\n buffer[#buffer + 1] = \"-\"\n totalSeconds = -totalSeconds\n maxComponents = maxComponents + 1\n end\n\n local showOnlyYears = totalSeconds > minTotalSecondsToShowOnlyYears\n\n local years = floor(totalSeconds / secondsInYear)\n if years > 0 then buffer[#buffer + 1] = years .. \"y\" end\n\n if #buffer < maxComponents and not showOnlyYears then\n local days = floor(totalSeconds % secondsInYear / secondsInDay)\n if days > 0 then buffer[#buffer + 1] = days .. \"d\" end\n end\n\n if #buffer < maxComponents and not showOnlyYears then\n local hours = floor(totalSeconds % secondsInDay / secondsInHour)\n if hours > 0 then buffer[#buffer + 1] = hours .. \"h\" end\n end\n\n if #buffer < maxComponents and not showOnlyYears then\n local minutes = floor(totalSeconds % secondsInHour / secondsInMinute)\n if minutes > 0 then buffer[#buffer + 1] = minutes .. \"m\" end\n end\n\n if #buffer < maxComponents and not showOnlyYears then\n local seconds = floor(totalSeconds % secondsInMinute)\n if seconds > 0 then buffer[#buffer + 1] = seconds .. \"s\" end\n end\n\n if #buffer == 0 then return \"0s\" end\n\n return concat(buffer, \" \")\n\nend\n\n\n\n\nfunction updateScreen()\n\nloc = vec3(core.getConstructWorldPos())\n\nlocal shipVelocity = vec3(core.getVelocity()):len() * 3.6\nlocal shipAcceleration = vec3(core.getVelocity()):len() * 3.6\nlocal time_to_distance = 0\nlocal display_selection = \"\"\n\nif selection == 1 then\n alioth = galaxyReference[0][2] ---uses Atlas functions\n distalioth = math.floor(alioth:getDistance(loc)/200000) ---uses getDistance functions----\n time_to_distance = distalioth * 200 / shipVelocity\n display_selection = \"alioth\"\nelseif selection == 2 then\n madis = vec3(17465536.000, 22665536.000, -34464.000)\n distmadis = string.format(\"%.2f\", math.sqrt((loc.x-madis.x)^2+(loc.y-madis.y)^2+(loc.z-madis.z)^2)/200000)\n time_to_distance = distmadis * 200 / shipVelocity\n display_selection = \"madis\"\nelseif selection == 3 then\n thades = vec3(29165536.000, 10865536.000, 65536.000)\n distthades = string.format(\"%.2f\", math.sqrt((loc.x-thades.x)^2+(loc.y-thades.y)^2+(loc.z-thades.z)^2)/200000)\n time_to_distance = distthades * 200 / shipVelocity\n display_selection = \"thades\"\nelseif selection == 4 then\n talemai = vec3(-13234464.000, 55765536.000, 465536.000)\n disttalemai = string.format(\"%.2f\", math.sqrt((loc.x-talemai.x)^2+(loc.y-talemai.y)^2+(loc.z-talemai.z)^2)/200000)\n time_to_distance = disttalemai * 200 / shipVelocity\n display_selection = \"talemai\"\nelseif selection == 5 then\n feli = vec3(-43534464.000, 22565536.000, -48934464.000)\n distfeli = string.format(\"%.2f\", math.sqrt((loc.x-feli.x)^2+(loc.y-feli.y)^2+(loc.z-feli.z)^2)/200000)\n time_to_distance = distfeli * 200 / shipVelocity\n display_selection = \"feli\"\nelseif selection == 6 then\n sicari = vec3(52765536.000, 27165536.000, 52065536.000)\n distsicari = string.format(\"%.2f\", math.sqrt((loc.x-sicari.x)^2+(loc.y-sicari.y)^2+(loc.z-sicari.z)^2)/200000)\n time_to_distance = distsicari * 200 / shipVelocity\n display_selection = \"sicari\"\nelseif selection == 7 then\n symeon = vec3(14165536.000, -85634464.000, -934464.000)\n distsymeon = string.format(\"%.2f\", math.sqrt((loc.x-symeon.x)^2+(loc.y-symeon.y)^2+(loc.z-symeon.z)^2)/200000)\n time_to_distance = distsymeon * 200 / shipVelocity\n display_selection = \"symeon\"\nelseif selection == 8 then\n sinnen = vec3(58665536.000, 29665536.000, 58165536.000)\n distsinnen = string.format(\"%.2f\", math.sqrt((loc.x-sinnen.x)^2+(loc.y-sinnen.y)^2+(loc.z-sinnen.z)^2)/200000)\n time_to_distance = distsinnen * 200 / shipVelocity\n display_selection = \"sinnen\"\nelseif selection == 9 then\n jago = vec3(-94134464.000, 12765536.000, -3634464.000)\n distjago = string.format(\"%.2f\", math.sqrt((loc.x-jago.x)^2+(loc.y-jago.y)^2+(loc.z-jago.z)^2)/200000)\n time_to_distance = distjago * 200 / shipVelocity\n display_selection = \"jago\"\nelseif selection == 10 then\n teoma = vec3(80865536.000, 54665536.000, -934464.000)\n distteoma = string.format(\"%.2f\", math.sqrt((loc.x-teoma.x)^2+(loc.y-teoma.y)^2+(loc.z-teoma.z)^2)/200000)\n time_to_distance = distteoma * 200 / shipVelocity\n display_selection = \"teoma\"\nelseif selection == 11 then\n ion = galaxyReference[0][120] ---uses Atlas functions\n distion = math.floor(ion:getDistance(loc)/200000) ---uses getDistance functions----\n time_to_distance = distion * 200 / shipVelocity\n display_selection = \"ion\"\nelseif selection == 12 then\n lacobus = vec3(98865536.000, -13534464.000, -934464.000)\n distlacobus = string.format(\"%.2f\", math.sqrt((loc.x-lacobus.x)^2+(loc.y-lacobus.y)^2+(loc.z-lacobus.z)^2)/200000)\n time_to_distance = distlacobus * 200 / shipVelocity\n display_selection = \"lacobus\"\nelse\n time_to_distance = sudistance * 200 / shipVelocity\n display_selection = \"none\"\nend\nshipVelocity = string.format(\"%.2f\", shipVelocity)\nwarpmath = math.floor(math.floor(core.getConstructMass()/ 1000) * sudistance * 0.00025)\n\ntime_to_distance_min = time_to_distance * 60\ntime_to_distance_min_sec = time_to_distance_min * 60\n\ntime_to_distance = formatTimeWithUnits (time_to_distance_min_sec, 3)\n\nhtml= ([[\n<svg class=\"bootstrap\" viewBox=\"0 0 1024 1024\" style=\"width:100%; height:100%\">\n\n<circle cx=\"500\" cy=\"500\" r=\"400\" stroke=\"#FFF\" stroke-width=\"3\" transform=\"\"></circle>\n<circle cx=\"500\" cy=\"500\" r=\"350\" stroke=\"#FFF\" stroke-width=\"3\" transform=\"\" stroke-opacity=\"0.2\"></circle>\n<circle cx=\"500\" cy=\"500\" r=\"300\" stroke=\"#FFF\" stroke-width=\"3\" transform=\"\"></circle><circle cx=\"500\" cy=\"500\" r=\"250\" stroke=\"#FFF\" stroke-width=\"3\" transform=\"\" stroke-opacity=\"0.2\"></circle>\n<circle cx=\"500\" cy=\"500\" r=\"200\" stroke=\"#FFF\" stroke-width=\"3\" transform=\"\"></circle><circle cx=\"500\" cy=\"500\" r=\"150\" stroke=\"#FFF\" stroke-width=\"3\" transform=\"\" stroke-opacity=\"0.2\"></circle>\n<circle cx=\"500\" cy=\"500\" r=\"100\" stroke=\"lightblue\" stroke-width=\"3\" transform=\"\"></circle><circle cx=\"500\" cy=\"500\" r=\"50\" stroke=\"lightblue\" stroke-width=\"3\" transform=\"\" stroke-opacity=\"0.2\"></circle>\n<circle cx=\"500\" cy=\"500\" r=\"20\" stroke=\"Orange\" stroke-width=\"2\" transform=\"\"></circle><text x=\"510\" y=\"510\" fill=\"Yellow\">Helios</text>\n<circle cx=\"-0.00\" cy=\"0\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle>\n<text x=\"-0.00\" y=\"0\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Alioth</text><circle cx=\"7.16\" cy=\"247.59\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle>\n<text x=\"7.16\" y=\"247.59\" transform=\"translate(480,480)\" fill=\"white\" font-size=\"20\">Ion</text><circle cx=\"35.41\" cy=\"214.09\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle>\n<text x=\"35.41\" y=\"214.09\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Symeon</text><circle cx=\"-33.09\" cy=\"-139.41\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle>\n<text x=\"-33.09\" y=\"-139.41\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Talemai</text><circle cx=\"202.16\" cy=\"-136.66\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle>\n<text x=\"202.16\" y=\"-136.66\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Teoma</text><circle cx=\"247.16\" cy=\"33.84\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle>\n<text x=\"247.16\" y=\"33.84\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Lacobus</text><circle cx=\"-108.84\" cy=\"-56.41\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle>\n<text x=\"-108.84\" y=\"-56.41\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Feli</text><circle cx=\"72.91\" cy=\"-27.16\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle>\n<text x=\"72.91\" y=\"-27.16\" transform=\"translate(500,485)\" fill=\"white\" font-size=\"20\">Thades</text><circle cx=\"43.66\" cy=\"-56.66\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle>\n<text x=\"43.66\" y=\"-56.66\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Madis</text><circle cx=\"-235.34\" cy=\"-31.91\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle>\n<text x=\"-235.34\" y=\"-31.91\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Jago</text><circle cx=\"131.91\" cy=\"-67.91\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle>\n<text x=\"131.91\" y=\"-67.91\" transform=\"translate(475,480)\" fill=\"white\" font-size=\"20\">Sicari</text><circle cx=\"146.66\" cy=\"-74.16\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle>\n<text x=\"146.66\" y=\"-74.16\" transform=\"translate(515,480)\" fill=\"white\" font-size=\"20\">Sinnen</text>\n<line stroke-linecap=\"undefined\" stroke-linejoin=\"undefined\" id=\"svg_1\" y2=\"]]..destY..[[\" x2=\"]]..destX..[[\" y1=\"]]..locY..[[\" x1=\"]]..locX..[[\" transform=\"translate(500,500)\" stroke-width=\"5\" stroke=\"#ff0000\" fill=\"none\"/>\n<circle cx=\"]]..locX..[[\" cy=\"]]..locY..[[\" r=\"3\" stroke=\"black\" stroke-width=\"1\" fill=\"limegreen\" transform=\"translate(500,500)\"></circle>\n<text x=\"]]..locX..[[\" y=\"]]..locY..[[\" transform=\"translate(500,500)\"\nfill=\"limegreen\" font-size= \"4.5vh\" font-weight= \"bold\">//SHIP POSITION</text>\n</svg>\n<svg class=\"bootstrap\" viewBox=\"0 0 1024 612\" style=\"width:100%; height:100%\">\n\n <g>\n <title>Layer 1</title>\n <g id=\"svg_24\">\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_8\" y=\"70\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Alioth :]]..distalioth..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_14\" y=\"170\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Madis :]]..distmadis..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_17\" y=\"270\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Thades :]]..distthades..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_20\" y=\"370\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Talemai :]]..disttalemai..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_23\" y=\"470\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Feli :]]..distfeli..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_26\" y=\"570\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Sicari :]]..distsicari..[[ SU</text>\n <g id=\"svg_12\">\n <rect rx=\"10\" id=\"svg_1\" height=\"50\" width=\"250\" y=\"30\" x=\"15\" stroke-width=\"10\" stroke=\"#FFF\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_3\" height=\"50\" width=\"250\" y=\"105\" x=\"15\" stroke-width=\"10\" stroke=\"#FFF\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_7\" height=\"50\" width=\"250\" y=\"180\" x=\"15\" stroke-width=\"10\" stroke=\"#FFF\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_9\" height=\"50\" width=\"250\" y=\"255\" x=\"15\" stroke-width=\"10\" stroke=\"#FFF\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_10\" height=\"50\" width=\"250\" y=\"330\" x=\"15\" stroke-width=\"10\" stroke=\"#FFF\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_11\" height=\"50\" width=\"250\" y=\"405\" x=\"15\" stroke-width=\"10\" stroke=\"#FFF\" fill=\"none\"/>\n </g>\n </g>\n <g id=\"svg_40\">\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_25\" y=\"70\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Symeon :]]..distsymeon..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_27\" y=\"170\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Sinnen :]]..distsinnen..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_28\" y=\"270\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Jago :]]..distjago..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_30\" y=\"370\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Teoma :]]..distteoma..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_31\" y=\"470\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Ion :]]..distion..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_32\" y=\"570\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Lacobus :]]..distlacobus..[[ SU</text>\n <g id=\"svg_39\">\n <rect rx=\"10\" id=\"svg_33\" height=\"50\" width=\"250\" y=\"30\" x=\"760\" stroke-width=\"10\" stroke=\"#FFF\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_34\" height=\"50\" width=\"250\" y=\"105\" x=\"760\" stroke-width=\"10\" stroke=\"#FFF\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_35\" height=\"50\" width=\"250\" y=\"180\" x=\"760\" stroke-width=\"10\" stroke=\"#FFF\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_36\" height=\"50\" width=\"250\" y=\"255\" x=\"760\" stroke-width=\"10\" stroke=\"#FFF\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_37\" height=\"50\" width=\"250\" y=\"330\" x=\"760\" stroke-width=\"10\" stroke=\"#FFF\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_38\" height=\"50\" width=\"250\" y=\"405\" x=\"760\" stroke-width=\"10\" stroke=\"#FFF\" fill=\"none\"/>\n </g>\n </g>\n </g>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"30\" id=\"svg_32\" y=\"700\" x=\"20\" stroke-width=\"0\" fill=\"LightBlue\">Est. Warp Cost: ]]..warpmath..[[</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"30\" id=\"svg_32\" y=\"750\" x=\"20\" stroke-width=\"0\" fill=\"LightBlue\">Construct Weight: ]]..math.floor(core.getConstructMass()/ 1000)..[[ tons</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"30\" id=\"svg_32\" y=\"700\" x=\"500\" stroke-width=\"0\" fill=\"LightBlue\">TTD: ]]..time_to_distance..[[ </text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"30\" id=\"svg_32\" y=\"750\" x=\"500\" stroke-width=\"0\" fill=\"LightBlue\">VELOC: ]]..shipVelocity..[[ km/h</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"30\" id=\"svg_32\" y=\"700\" x=\"900\" stroke-width=\"0\" fill=\"LightBlue\">DEST: ]]..display_selection..[[ </text>\n\n</svg>\n\n ]])\n\nscreen.setHTML(html)\n--screen2.setHTML(html)\nend\nunit.setTimer(\"spacemap\",.08)\n\n","filter":{"args":[],"signature":"start()","slotKey":"-1"},"key":"2"},{"code":"updateScreen()","filter":{"args":[{"value":"spacemap"}],"signature":"tick(timerId)","slotKey":"-1"},"key":"3"}],"methods":[],"events":[]}
----Older Version In Multiple formats for Learning Purposes. DU IT
Space Map with Warp Calculation
Credits to All of DU Lua Community
Requirements:
1 Dynamic Construct
1 Screen
1 Program Board
Link Screen then Core
Two Versions are available and do the same thing.
One uses variables and math with some built in functions from Lua to get the values.
One uses Functions from JayleBreak's atlas and functions to get the values.
*KNOWN BUGS*
----On fresh login, Core has to be ran one time to send Construct weight data over the server, otherwise math will be wrong.
So sit down in pilot seat one time and then run programming board. After that its always set. ---Server Bug
----Currently has Bug with Screen Flickers on half of the svg during setHTML redraw update-- 9/23 Patch
Planets are organized similar to DU ingame map and are stationary svg.
---------- Math and Variables Version---------
---Space Map
---Unit Start
MapScreenButtons = {}
MapScreenMouseX = 0
MapScreenMouseY = 0
MapScreenMouseDown = false
MapScreenButtonSelected = 0
local worldPos = vec3(core.getConstructWorldPos())
local locX = (worldPos.x/400000)
local locY = (worldPos.y/400000)*(-1)
local destX = 0
local destY = 0
local sudistance = 0
local loc = vec3(core.getConstructWorldPos())
local ion = vec3(2865536.000, -99034464.000, -934464.000)
local thades = vec3(29165536.000, 10865536.000, 65536.000)
local sinnen = vec3(58665536.000, 29665536.000, 58165536.000)
local alioth = vec3(-8.000, -8.000, -126303.000)
local madis = vec3(17465536.000, 22665536.000, -34464.000)
local jago = vec3(-94134464.000, 12765536.000, -3634464.000)
local symeon = vec3(14165536.000, -85634464.000, -934464.000)
local lacobus = vec3(98865536.000, -13534464.000, -934464.000)
local teoma = vec3(80865536.000, 54665536.000, -934464.000)
local feli = vec3(-43534464.000, 22565536.000, -48934464.000)
local talemai = vec3(-13234464.000, 55765536.000, 465536.000)
local sicari = vec3(52765536.000, 27165536.000, 52065536.000)
local distion = string.format("%.2f", math.sqrt((loc.x-ion.x)^2+(loc.y-ion.y)^2+(loc.z-ion.z)^2)/200000)
local distthades = string.format("%.2f", math.sqrt((loc.x-thades.x)^2+(loc.y-thades.y)^2+(loc.z-thades.z)^2)/200000)
local distalioth = string.format("%.2f", math.sqrt((loc.x-alioth.x)^2+(loc.y-alioth.y)^2+(loc.z-alioth.z)^2)/200000)
local distmadis = string.format("%.2f", math.sqrt((loc.x-madis.x)^2+(loc.y-madis.y)^2+(loc.z-madis.z)^2)/200000)
local distjago = string.format("%.2f", math.sqrt((loc.x-jago.x)^2+(loc.y-jago.y)^2+(loc.z-jago.z)^2)/200000)
local distlacobus = string.format("%.2f", math.sqrt((loc.x-lacobus.x)^2+(loc.y-lacobus.y)^2+(loc.z-lacobus.z)^2)/200000)
local distteoma = string.format("%.2f", math.sqrt((loc.x-teoma.x)^2+(loc.y-teoma.y)^2+(loc.z-teoma.z)^2)/200000)
local distsymeon = string.format("%.2f", math.sqrt((loc.x-symeon.x)^2+(loc.y-symeon.y)^2+(loc.z-symeon.z)^2)/200000)
local distfeli = string.format("%.2f", math.sqrt((loc.x-feli.x)^2+(loc.y-feli.y)^2+(loc.z-feli.z)^2)/200000)
local distsinnen = string.format("%.2f", math.sqrt((loc.x-sinnen.x)^2+(loc.y-sinnen.y)^2+(loc.z-sinnen.z)^2)/200000)
local disttalemai = string.format("%.2f", math.sqrt((loc.x-talemai.x)^2+(loc.y-talemai.y)^2+(loc.z-talemai.z)^2)/200000)
local distsicari = string.format("%.2f", math.sqrt((loc.x-sicari.x)^2+(loc.y-sicari.y)^2+(loc.z-sicari.z)^2)/200000)
for i = 1,1 do
local button = {id = ("b"..1), enabled=true, td="<td>", top=2/100, bottom=13/100, left=1/100, right=28/100}
table.insert(MapScreenButtons, button)
end
for i = 2,2 do
local button = {id = ("b"..2), enabled=true, td="<td>", top=15/100, bottom=26/100, left=1/100, right=30/100}
table.insert(MapScreenButtons, button)
end
for i = 3,3 do
local button = {id = ("b"..3), enabled=true, td="<td>", top=27/100, bottom=38/100, left=1/100, right=28/100}
table.insert(MapScreenButtons, button)
end
for i = 4,4 do
local button = {id = ("b"..4), enabled=true, td="<td>", top=39/100, bottom=50/100, left=1/100, right=28/100}
table.insert(MapScreenButtons, button)
end
for i = 5,5 do
local button = {id = ("b"..5), enabled=true, td="<td>", top=51/100, bottom=62/100, left=1/100, right=28/100}
table.insert(MapScreenButtons, button)
end
for i = 6,6 do
local button = {id = ("b"..6), enabled=true, td="<td>", top=64/100, bottom=75/100, left=1/100, right=28/100}
table.insert(MapScreenButtons, button)
end
for i = 7,7 do
local button = {id = ("b"..7), enabled=true, td="<td>", top=2/100, bottom=13/100, left=75/100, right=100/100}
table.insert(MapScreenButtons, button)
end
for i = 8,8 do
local button = {id = ("b"..8), enabled=true, td="<td>", top=15/100, bottom=26/100, left=75/100, right=100/100}
table.insert(MapScreenButtons, button)
end
for i = 9,9 do
local button = {id = ("b"..9), enabled=true, td="<td>", top=27/100, bottom=38/100, left=75/100, right=100/100}
table.insert(MapScreenButtons, button)
end
for i = 10,10 do
local button = {id = ("b"..10), enabled=true, td="<td>", top=39/100, bottom=50/100, left=75/100, right=100/100}
table.insert(MapScreenButtons, button)
end
for i = 11,11 do
local button = {id = ("b"..11), enabled=true, td="<td>", top=51/100, bottom=62/100, left=75/100, right=100/100}
table.insert(MapScreenButtons, button)
end
for i = 12,12 do
local button = {id = ("b"..12), enabled=true, td="<td>", top=64/100, bottom=75/100, left=75/100, right=100/100}
table.insert(MapScreenButtons, button)
end
for i = 13,13 do
local button = {id = ("b"..13), enabled=true, td="<td>", top=90/100, bottom=100/100, left=1/100, right=18/100}
table.insert(MapScreenButtons, button)
end
function evaluateButtons()
local selected = 0
if #MapScreenButtons >= 1 then
-- Set button styles
for i, button in ipairs(MapScreenButtons) do
if button.left < MapScreenMouseX and MapScreenMouseX < button.right and button.top < MapScreenMouseY and MapScreenMouseY < button.bottom then
if MapScreenMouseDown and MapScreenButtonSelected == i then
end
selected = i
end
if not button.enabled then
end
end
end
return selected
end
function onButtonDown(buttonNo)
local button = MapScreenButtons[buttonNo]
if not button or not button.enabled then
return
end
end
function onButtonUp(buttonNo)
local button = MapScreenButtons[buttonNo]
if not button or not button.enabled then
return
end
function onClick(buttonNo)
local button = MapScreenButtons[buttonNo]
if not button or not button.enabled then
return
end
end
if buttonNo == 1 then
destX = 0
destY = 0
sudistance = distalioth
elseif buttonNo == 2 then
destX = 43
destY = -56
sudistance = distmadis
elseif buttonNo == 3 then
destX = 73
destY = -27
sudistance = distthades
elseif buttonNo == 4 then
destX = -33
destY = -139
sudistance = disttalemai
elseif buttonNo == 5 then
destX = -109
destY = -56
sudistance = distfeli
elseif buttonNo == 6 then
destX = 131
destY = -68
sudistance = distsicari
elseif buttonNo == 7 then
destX = 35
destY = 214
sudistance = distsymeon
elseif buttonNo == 8 then
destX = 146
destY = -74
sudistance = distsinnen
elseif buttonNo == 9 then
destX = -235
destY = -32
sudistance = distjago
elseif buttonNo == 10 then
destX = 202
destY = -137
sudistance = distteoma
elseif buttonNo == 11 then
destX = 7
destY = 247
sudistance = distion
elseif buttonNo == 12 then
destX = 247
destY = 34
sudistance = distlacobus
elseif buttonNo == 13 then
unit.exit()
end
end
function updateScreen()
warpmath = math.floor(math.floor(core.getConstructMass()/ 1000) * sudistance * 0.00025)
html= ([[
<svg class="bootstrap" viewBox="0 0 1024 1024" style="width:100%; height:100%">
<circle cx="500" cy="500" r="400" stroke="darkgreen" stroke-width="3" transform=""></circle><circle cx="500" cy="500" r="350" stroke="darkgreen" stroke-width="3" transform="" stroke-opacity="0.2"></circle><circle cx="500" cy="500" r="300" stroke="darkgreen" stroke-width="3" transform=""></circle><circle cx="500" cy="500" r="250" stroke="darkgreen" stroke-width="3" transform="" stroke-opacity="0.2"></circle><circle cx="500" cy="500" r="200" stroke="darkgreen" stroke-width="3" transform=""></circle><circle cx="500" cy="500" r="150" stroke="darkgreen" stroke-width="3" transform="" stroke-opacity="0.2"></circle><circle cx="500" cy="500" r="100" stroke="lightblue" stroke-width="3" transform=""></circle><circle cx="500" cy="500" r="50" stroke="lightblue" stroke-width="3" transform="" stroke-opacity="0.2"></circle><circle cx="500" cy="500" r="20" stroke="Orange" stroke-width="2" transform=""></circle><text x="510" y="510" fill="Yellow">Helios</text><circle cx="-0.00" cy="0" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="-0.00" y="0" transform="translate(500,480)" fill="white" font-size="20">Alioth</text><circle cx="7.16" cy="247.59" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="7.16" y="247.59" transform="translate(480,480)" fill="white" font-size="20">Ion</text><circle cx="35.41" cy="214.09" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="35.41" y="214.09" transform="translate(500,480)" fill="white" font-size="20">Symeon</text><circle cx="-33.09" cy="-139.41" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="-33.09" y="-139.41" transform="translate(500,480)" fill="white" font-size="20">Talemai</text><circle cx="202.16" cy="-136.66" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="202.16" y="-136.66" transform="translate(500,480)" fill="white" font-size="20">Teoma</text><circle cx="247.16" cy="33.84" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="247.16" y="33.84" transform="translate(500,480)" fill="white" font-size="20">Lacobus</text><circle cx="-108.84" cy="-56.41" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="-108.84" y="-56.41" transform="translate(500,480)" fill="white" font-size="20">Feli</text><circle cx="72.91" cy="-27.16" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="72.91" y="-27.16" transform="translate(500,485)" fill="white" font-size="20">Thades</text><circle cx="43.66" cy="-56.66" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="43.66" y="-56.66" transform="translate(500,480)" fill="white" font-size="20">Madis</text><circle cx="-235.34" cy="-31.91" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="-235.34" y="-31.91" transform="translate(500,480)" fill="white" font-size="20">Jago</text><circle cx="131.91" cy="-67.91" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="131.91" y="-67.91" transform="translate(475,480)" fill="white" font-size="20">Sicari</text><circle cx="146.66" cy="-74.16" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="146.66" y="-74.16" transform="translate(515,480)" fill="white" font-size="20">Sinnen</text>
<line stroke-linecap="undefined" stroke-linejoin="undefined" id="svg_1" y2="]]..destY..[[" x2="]]..destX..[[" y1="]]..locY..[[" x1="]]..locX..[[" transform="translate(500,500)" stroke-width="5" stroke="#ff0000" fill="none"/>
<circle cx="]]..locX..[[" cy="]]..locY..[[" r="3" stroke="black" stroke-width="1" fill="limegreen" transform="translate(500,500)"></circle>
<text x="]]..locX..[[" y="]]..locY..[[" transform="translate(500,500)"
fill="limegreen" font-size= "4.5vh" font-weight= "bold">//SHIP POSITION</text>
</svg>
<svg class="bootstrap" viewBox="0 0 1024 612" style="width:100%; height:100%">
<g>
<title>Layer 1</title>
<g id="svg_24">
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_8" y="70" x="55" stroke-width="0" fill="Yellow">Alioth :]]..distalioth..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_14" y="170" x="55" stroke-width="0" fill="Yellow">Madis :]]..distmadis..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_17" y="270" x="55" stroke-width="0" fill="Yellow">Thades :]]..distthades..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_20" y="370" x="55" stroke-width="0" fill="Yellow">Talemai :]]..disttalemai..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_23" y="470" x="55" stroke-width="0" fill="Yellow">Feli :]]..distfeli..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_26" y="570" x="55" stroke-width="0" fill="Yellow">Sicari :]]..distsicari..[[ SU</text>
<g id="svg_12">
<rect rx="10" id="svg_1" height="50" width="250" y="30" x="15" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_3" height="50" width="250" y="105" x="15" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_7" height="50" width="250" y="180" x="15" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_9" height="50" width="250" y="255" x="15" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_10" height="50" width="250" y="330" x="15" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_11" height="50" width="250" y="405" x="15" stroke-width="20" stroke="#00ff00" fill="none"/>
</g>
</g>
<g id="svg_40">
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_25" y="70" x="997.163642" stroke-width="0" fill="Yellow">Symeon :]]..distsymeon..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_27" y="170" x="997.163642" stroke-width="0" fill="Yellow">Sinnen :]]..distsinnen..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_28" y="270" x="997.163642" stroke-width="0" fill="Yellow">Jago :]]..distjago..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_30" y="370" x="997.163642" stroke-width="0" fill="Yellow">Teoma :]]..distteoma..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_31" y="470" x="997.163642" stroke-width="0" fill="Yellow">Ion :]]..distion..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_32" y="570" x="997.163642" stroke-width="0" fill="Yellow">Lacobus :]]..distlacobus..[[ SU</text>
<g id="svg_39">
<rect rx="10" id="svg_33" height="50" width="250" y="30" x="760" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_34" height="50" width="250" y="105" x="760" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_35" height="50" width="250" y="180" x="760" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_36" height="50" width="250" y="255" x="760" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_37" height="50" width="250" y="330" x="760" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_38" height="50" width="250" y="405" x="760" stroke-width="20" stroke="#00ff00" fill="none"/>
</g>
</g>
</g>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="30" id="svg_32" y="700" x="20" stroke-width="0" fill="LightBlue">Est. Warp Cost: ]]..warpmath..[[</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="30" id="svg_32" y="750" x="20" stroke-width="0" fill="LightBlue">Construct Weight: ]]..math.floor(core.getConstructMass()/ 1000)..[[ tons</text>
</svg>
]])
screen.setHTML(html)
end
unit.setTimer("spacemap",.08)
---Unit Tick spacemap
updateScreen()
---MouseDown *,*
MapScreenMouseX = x
MapScreenMouseY = y
MapScreenMouseDown = true
MapScreenButtonSelected = evaluateButtons()
onButtonDown(MapScreenButtonSelected)
---MouseUp *,*
MapScreenMouseX = x
MapScreenMouseY = y
MapScreenMouseDown = false
local buttonNo = evaluateButtons()
if MapScreenButtonSelected > 0 and MapScreenButtonSelected == buttonNo then
onButtonUp(buttonNo)
onClick(buttonNo)
end
MapScreenButtonSelected = -buttonNo
Json Paste
{"slots":{"0":{"name":"screen","type":{"events":[],"methods":[]}},"1":{"name":"core","type":{"events":[],"methods":[]}},"2":{"name":"slot3","type":{"events":[],"methods":[]}},"3":{"name":"slot4","type":{"events":[],"methods":[]}},"4":{"name":"slot5","type":{"events":[],"methods":[]}},"5":{"name":"slot6","type":{"events":[],"methods":[]}},"6":{"name":"slot7","type":{"events":[],"methods":[]}},"7":{"name":"slot8","type":{"events":[],"methods":[]}},"8":{"name":"slot9","type":{"events":[],"methods":[]}},"9":{"name":"slot10","type":{"events":[],"methods":[]}},"-1":{"name":"unit","type":{"events":[],"methods":[]}},"-2":{"name":"system","type":{"events":[],"methods":[]}},"-3":{"name":"library","type":{"events":[],"methods":[]}}},"handlers":[{"code":"MapScreenMouseX = x\nMapScreenMouseY = y\nMapScreenMouseDown = false\nlocal buttonNo = evaluateButtons()\nif MapScreenButtonSelected > 0 and MapScreenButtonSelected == buttonNo then\n onButtonUp(buttonNo)\n onClick(buttonNo)\nend\nMapScreenButtonSelected = -buttonNo","filter":{"args":[{"variable":"*"},{"variable":"*"}],"signature":"mouseUp(x,y)","slotKey":"0"},"key":"0"},{"code":"MapScreenMouseX = x\nMapScreenMouseY = y\nMapScreenMouseDown = true\nMapScreenButtonSelected = evaluateButtons()\nonButtonDown(MapScreenButtonSelected)\n","filter":{"args":[{"variable":"*"},{"variable":"*"}],"signature":"mouseDown(x,y)","slotKey":"0"},"key":"1"},{"code":"MapScreenButtons = {}\nMapScreenMouseX = 0\nMapScreenMouseY = 0\nMapScreenMouseDown = false\nMapScreenButtonSelected = 0\n\n\n\nlocal worldPos = vec3(core.getConstructWorldPos())\nlocal locX = (worldPos.x/400000)\nlocal locY = (worldPos.y/400000)*(-1)\nlocal destX = 0\nlocal destY = 0\nlocal sudistance = 0\nlocal loc = vec3(core.getConstructWorldPos())\nlocal ion = vec3(2865536.000, -99034464.000, -934464.000)\nlocal thades = vec3(29165536.000, 10865536.000, 65536.000)\nlocal sinnen = vec3(58665536.000, 29665536.000, 58165536.000)\nlocal alioth = vec3(-8.000, -8.000, -126303.000)\nlocal madis = vec3(17465536.000, 22665536.000, -34464.000)\nlocal jago = vec3(-94134464.000, 12765536.000, -3634464.000)\nlocal symeon = vec3(14165536.000, -85634464.000, -934464.000)\nlocal lacobus = vec3(98865536.000, -13534464.000, -934464.000)\nlocal teoma = vec3(80865536.000, 54665536.000, -934464.000)\nlocal feli = vec3(-43534464.000, 22565536.000, -48934464.000)\nlocal talemai = vec3(-13234464.000, 55765536.000, 465536.000)\nlocal sicari = vec3(52765536.000, 27165536.000, 52065536.000)\nlocal distion = string.format(\"%.2f\", math.sqrt((loc.x-ion.x)^2+(loc.y-ion.y)^2+(loc.z-ion.z)^2)/200000)\nlocal distthades = string.format(\"%.2f\", math.sqrt((loc.x-thades.x)^2+(loc.y-thades.y)^2+(loc.z-thades.z)^2)/200000)\nlocal distalioth = string.format(\"%.2f\", math.sqrt((loc.x-alioth.x)^2+(loc.y-alioth.y)^2+(loc.z-alioth.z)^2)/200000)\nlocal distmadis = string.format(\"%.2f\", math.sqrt((loc.x-madis.x)^2+(loc.y-madis.y)^2+(loc.z-madis.z)^2)/200000)\nlocal distjago = string.format(\"%.2f\", math.sqrt((loc.x-jago.x)^2+(loc.y-jago.y)^2+(loc.z-jago.z)^2)/200000)\nlocal distlacobus = string.format(\"%.2f\", math.sqrt((loc.x-lacobus.x)^2+(loc.y-lacobus.y)^2+(loc.z-lacobus.z)^2)/200000)\nlocal distteoma = string.format(\"%.2f\", math.sqrt((loc.x-teoma.x)^2+(loc.y-teoma.y)^2+(loc.z-teoma.z)^2)/200000)\nlocal distsymeon = string.format(\"%.2f\", math.sqrt((loc.x-symeon.x)^2+(loc.y-symeon.y)^2+(loc.z-symeon.z)^2)/200000)\nlocal distfeli = string.format(\"%.2f\", math.sqrt((loc.x-feli.x)^2+(loc.y-feli.y)^2+(loc.z-feli.z)^2)/200000)\nlocal distsinnen = string.format(\"%.2f\", math.sqrt((loc.x-sinnen.x)^2+(loc.y-sinnen.y)^2+(loc.z-sinnen.z)^2)/200000)\nlocal disttalemai = string.format(\"%.2f\", math.sqrt((loc.x-talemai.x)^2+(loc.y-talemai.y)^2+(loc.z-talemai.z)^2)/200000)\nlocal distsicari = string.format(\"%.2f\", math.sqrt((loc.x-sicari.x)^2+(loc.y-sicari.y)^2+(loc.z-sicari.z)^2)/200000)\n\n\n\n for i = 1,1 do\n local button = {id = (\"b\"..1), enabled=true, td=\"<td>\", top=2/100, bottom=13/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 2,2 do\n local button = {id = (\"b\"..2), enabled=true, td=\"<td>\", top=15/100, bottom=26/100, left=1/100, right=30/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 3,3 do\n local button = {id = (\"b\"..3), enabled=true, td=\"<td>\", top=27/100, bottom=38/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 4,4 do \n local button = {id = (\"b\"..4), enabled=true, td=\"<td>\", top=39/100, bottom=50/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 5,5 do \n local button = {id = (\"b\"..5), enabled=true, td=\"<td>\", top=51/100, bottom=62/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 6,6 do \n local button = {id = (\"b\"..6), enabled=true, td=\"<td>\", top=64/100, bottom=75/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 7,7 do \n local button = {id = (\"b\"..7), enabled=true, td=\"<td>\", top=2/100, bottom=13/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 8,8 do \n local button = {id = (\"b\"..8), enabled=true, td=\"<td>\", top=15/100, bottom=26/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 9,9 do \n local button = {id = (\"b\"..9), enabled=true, td=\"<td>\", top=27/100, bottom=38/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 10,10 do \n local button = {id = (\"b\"..10), enabled=true, td=\"<td>\", top=39/100, bottom=50/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 11,11 do \n local button = {id = (\"b\"..11), enabled=true, td=\"<td>\", top=51/100, bottom=62/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 12,12 do \n local button = {id = (\"b\"..12), enabled=true, td=\"<td>\", top=64/100, bottom=75/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 13,13 do \n local button = {id = (\"b\"..13), enabled=true, td=\"<td>\", top=90/100, bottom=100/100, left=1/100, right=18/100}\n table.insert(MapScreenButtons, button)\nend\nfunction evaluateButtons()\n local selected = 0\n \n if #MapScreenButtons >= 1 then\n -- Set button styles\n for i, button in ipairs(MapScreenButtons) do\n if button.left < MapScreenMouseX and MapScreenMouseX < button.right and button.top < MapScreenMouseY and MapScreenMouseY < button.bottom then\n if MapScreenMouseDown and MapScreenButtonSelected == i then\n end\n selected = i\n end\n if not button.enabled then\n end\n\n end\n end\n return selected\nend\n\nfunction onButtonDown(buttonNo)\n local button = MapScreenButtons[buttonNo] \n if not button or not button.enabled then\n\treturn\n end\nend\nfunction onButtonUp(buttonNo)\n local button = MapScreenButtons[buttonNo] \n if not button or not button.enabled then\n return\n end\nfunction onClick(buttonNo)\n local button = MapScreenButtons[buttonNo] \n if not button or not button.enabled then\n return\n end\nend\n if buttonNo == 1 then\ndestX = 0\ndestY = 0\nsudistance = distalioth\n elseif buttonNo == 2 then\ndestX = 43\ndestY = -56\nsudistance = distmadis\n elseif buttonNo == 3 then\ndestX = 73\ndestY = -27\nsudistance = distthades \n elseif buttonNo == 4 then\ndestX = -33\ndestY = -139\nsudistance = disttalemai\n elseif buttonNo == 5 then\ndestX = -109\ndestY = -56\nsudistance = distfeli \n elseif buttonNo == 6 then\ndestX = 131\ndestY = -68\nsudistance = distsicari \n elseif buttonNo == 7 then\ndestX = 35\ndestY = 214\nsudistance = distsymeon\n elseif buttonNo == 8 then\ndestX = 146\ndestY = -74\nsudistance = distsinnen \n elseif buttonNo == 9 then\ndestX = -235\ndestY = -32\nsudistance = distjago \n elseif buttonNo == 10 then\ndestX = 202\ndestY = -137\nsudistance = distteoma \n elseif buttonNo == 11 then\ndestX = 7\ndestY = 247\nsudistance = distion \n elseif buttonNo == 12 then\ndestX = 247\ndestY = 34\nsudistance = distlacobus\n elseif buttonNo == 13 then\n unit.exit()\n end\nend\n\nfunction updateScreen() \nwarpmath = math.floor(math.floor(core.getConstructMass()/ 1000) * sudistance * 0.00025)\nhtml= ([[\n<svg class=\"bootstrap\" viewBox=\"0 0 1024 1024\" style=\"width:100%; height:100%\"> \n<circle cx=\"500\" cy=\"500\" r=\"400\" stroke=\"darkgreen\" stroke-width=\"3\" transform=\"\"></circle><circle cx=\"500\" cy=\"500\" r=\"350\" stroke=\"darkgreen\" stroke-width=\"3\" transform=\"\" stroke-opacity=\"0.2\"></circle><circle cx=\"500\" cy=\"500\" r=\"300\" stroke=\"darkgreen\" stroke-width=\"3\" transform=\"\"></circle><circle cx=\"500\" cy=\"500\" r=\"250\" stroke=\"darkgreen\" stroke-width=\"3\" transform=\"\" stroke-opacity=\"0.2\"></circle><circle cx=\"500\" cy=\"500\" r=\"200\" stroke=\"darkgreen\" stroke-width=\"3\" transform=\"\"></circle><circle cx=\"500\" cy=\"500\" r=\"150\" stroke=\"darkgreen\" stroke-width=\"3\" transform=\"\" stroke-opacity=\"0.2\"></circle><circle cx=\"500\" cy=\"500\" r=\"100\" stroke=\"lightblue\" stroke-width=\"3\" transform=\"\"></circle><circle cx=\"500\" cy=\"500\" r=\"50\" stroke=\"lightblue\" stroke-width=\"3\" transform=\"\" stroke-opacity=\"0.2\"></circle><circle cx=\"500\" cy=\"500\" r=\"20\" stroke=\"Orange\" stroke-width=\"2\" transform=\"\"></circle><text x=\"510\" y=\"510\" fill=\"Yellow\">Helios</text><circle cx=\"-0.00\" cy=\"0\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"-0.00\" y=\"0\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Alioth</text><circle cx=\"7.16\" cy=\"247.59\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"7.16\" y=\"247.59\" transform=\"translate(480,480)\" fill=\"white\" font-size=\"20\">Ion</text><circle cx=\"35.41\" cy=\"214.09\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"35.41\" y=\"214.09\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Symeon</text><circle cx=\"-33.09\" cy=\"-139.41\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"-33.09\" y=\"-139.41\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Talemai</text><circle cx=\"202.16\" cy=\"-136.66\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"202.16\" y=\"-136.66\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Teoma</text><circle cx=\"247.16\" cy=\"33.84\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"247.16\" y=\"33.84\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Lacobus</text><circle cx=\"-108.84\" cy=\"-56.41\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"-108.84\" y=\"-56.41\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Feli</text><circle cx=\"72.91\" cy=\"-27.16\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"72.91\" y=\"-27.16\" transform=\"translate(500,485)\" fill=\"white\" font-size=\"20\">Thades</text><circle cx=\"43.66\" cy=\"-56.66\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"43.66\" y=\"-56.66\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Madis</text><circle cx=\"-235.34\" cy=\"-31.91\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"-235.34\" y=\"-31.91\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Jago</text><circle cx=\"131.91\" cy=\"-67.91\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"131.91\" y=\"-67.91\" transform=\"translate(475,480)\" fill=\"white\" font-size=\"20\">Sicari</text><circle cx=\"146.66\" cy=\"-74.16\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"146.66\" y=\"-74.16\" transform=\"translate(515,480)\" fill=\"white\" font-size=\"20\">Sinnen</text>\n<line stroke-linecap=\"undefined\" stroke-linejoin=\"undefined\" id=\"svg_1\" y2=\"]]..destY..[[\" x2=\"]]..destX..[[\" y1=\"]]..locY..[[\" x1=\"]]..locX..[[\" transform=\"translate(500,500)\" stroke-width=\"5\" stroke=\"#ff0000\" fill=\"none\"/> \n<circle cx=\"]]..locX..[[\" cy=\"]]..locY..[[\" r=\"3\" stroke=\"black\" stroke-width=\"1\" fill=\"limegreen\" transform=\"translate(500,500)\"></circle>\n<text x=\"]]..locX..[[\" y=\"]]..locY..[[\" transform=\"translate(500,500)\" \nfill=\"limegreen\" font-size= \"4.5vh\" font-weight= \"bold\">//SHIP POSITION</text>\n</svg>\n<svg class=\"bootstrap\" viewBox=\"0 0 1024 612\" style=\"width:100%; height:100%\">\n <g>\n <title>Layer 1</title>\n <g id=\"svg_24\">\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_8\" y=\"70\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Alioth :]]..distalioth..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_14\" y=\"170\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Madis :]]..distmadis..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_17\" y=\"270\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Thades :]]..distthades..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_20\" y=\"370\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Talemai :]]..disttalemai..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_23\" y=\"470\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Feli :]]..distfeli..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_26\" y=\"570\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Sicari :]]..distsicari..[[ SU</text>\n <g id=\"svg_12\">\n <rect rx=\"10\" id=\"svg_1\" height=\"50\" width=\"250\" y=\"30\" x=\"15\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_3\" height=\"50\" width=\"250\" y=\"105\" x=\"15\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_7\" height=\"50\" width=\"250\" y=\"180\" x=\"15\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_9\" height=\"50\" width=\"250\" y=\"255\" x=\"15\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_10\" height=\"50\" width=\"250\" y=\"330\" x=\"15\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_11\" height=\"50\" width=\"250\" y=\"405\" x=\"15\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n </g>\n </g>\n <g id=\"svg_40\">\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_25\" y=\"70\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Symeon :]]..distsymeon..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_27\" y=\"170\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Sinnen :]]..distsinnen..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_28\" y=\"270\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Jago :]]..distjago..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_30\" y=\"370\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Teoma :]]..distteoma..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_31\" y=\"470\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Ion :]]..distion..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_32\" y=\"570\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Lacobus :]]..distlacobus..[[ SU</text>\n <g id=\"svg_39\">\n <rect rx=\"10\" id=\"svg_33\" height=\"50\" width=\"250\" y=\"30\" x=\"760\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_34\" height=\"50\" width=\"250\" y=\"105\" x=\"760\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_35\" height=\"50\" width=\"250\" y=\"180\" x=\"760\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_36\" height=\"50\" width=\"250\" y=\"255\" x=\"760\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_37\" height=\"50\" width=\"250\" y=\"330\" x=\"760\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_38\" height=\"50\" width=\"250\" y=\"405\" x=\"760\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n </g>\n </g>\n </g>\n<text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"30\" id=\"svg_32\" y=\"700\" x=\"20\" stroke-width=\"0\" fill=\"LightBlue\">Est. Warp Cost: ]]..warpmath..[[</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"30\" id=\"svg_32\" y=\"750\" x=\"20\" stroke-width=\"0\" fill=\"LightBlue\">Construct Weight: ]]..math.floor(core.getConstructMass()/ 1000)..[[ tons</text>\n \n</svg> \n ]])\nscreen.setHTML(html)\nend\nunit.setTimer(\"spacemap\",.08)\n\n","filter":{"args":[],"signature":"start()","slotKey":"-1"},"key":"2"},{"code":"updateScreen()","filter":{"args":[{"value":"spacemap"}],"signature":"tick(timerId)","slotKey":"-1"},"key":"3"}],"methods":[],"events":[]}
---------- JayleBreak Atlas and Functions Version---------
function Atlas()
return {
[0] = {
[1]={
GM=6930729684,
bodyId=1,
center={x=17465536.000,y=22665536.000,z=-34464.000},
name='Madis',
planetarySystemId=0,
radius=44300
},
[2]={
GM=157470826617,
bodyId=2,
center={x=-8.000,y=-8.000,z=-126303.000},
name='Alioth',
planetarySystemId=0,
radius=126068
},
[3]={
GM=11776905000,
bodyId=3,
center={x=29165536.000,y=10865536.000,z=65536.000},
name='Thades',
planetarySystemId=0,
radius=49000
},
[4]={
GM=14893847582,
bodyId=4,
center={x=-13234464.000,y=55765536.000,z=465536.000},
name='Talemai',
planetarySystemId=0,
radius=57450
},
[5]={
GM=16951680000,
bodyId=5,
center={x=-43534464.000,y=22565536.000,z=-48934464.000},
name='Feli',
planetarySystemId=0,
radius=60000
},
[6]={
GM=10502547741,
bodyId=6,
center={x=52765536.000,y=27165538.000,z=52065535.000},
name='Sicari',
planetarySystemId=0,
radius=51100
},
[7]={
GM=13033380591,
bodyId=7,
center={x=58665538.000,y=29665535.000,z=58165535.000},
name='Sinnen',
planetarySystemId=0,
radius=54950
},
[8]={
GM=18477723600,
bodyId=8,
center={x=80865538.000,y=54665536.000,z=-934463.940},
name='Teoma',
planetarySystemId=0,
radius=62000
},
[9]={
GM=18606274330,
bodyId=9,
center={x=-94134462.000,y=12765534.000,z=-3634464.000},
name='Jago',
planetarySystemId=0,
radius=61590
},
[10]={
GM=78480000,
bodyId=10,
center={x=17448118.224,y=22966846.286,z=143078.820},
name='Madis Moon 1',
planetarySystemId=0,
radius=10000
},
[11]={
GM=237402000,
bodyId=11,
center={x=17194626.000,y=22243633.880,z=-214962.810},
name='Madis Moon 2',
planetarySystemId=0,
radius=11000
},
[12]={
GM=265046609,
bodyId=12,
center={x=17520614.000,y=22184730.000,z=-309989.990},
name='Madis Moon 3',
planetarySystemId=0,
radius=15005
},
[21]={
GM=2118960000,
bodyId=21,
center={x=457933.000,y=-1509011.000,z=115524.000},
name='Alioth Moon 1',
planetarySystemId=0,
radius=30000
},
[22]={
GM=2165833514,
bodyId=22,
center={x=-1692694.000,y=729681.000,z=-411464.000},
name='Alioth Moon 4',
planetarySystemId=0,
radius=30330
},
[26]={
GM=68234043600,
bodyId=26,
center={x=-1404835.000,y=562655.000,z=-285074.000},
name='Sanctuary',
planetarySystemId=0,
radius=83400
},
[30]={
GM=211564034,
bodyId=30,
center={x=29214402.000,y=10907080.695,z=433858.200},
name='Thades Moon 1',
planetarySystemId=0,
radius=14002
},
[31]={
GM=264870000,
bodyId=31,
center={x=29404193.000,y=10432768.000,z=19554.131},
name='Thades Moon 2',
planetarySystemId=0,
radius=15000
},
[40]={
GM=141264000,
bodyId=40,
center={x=-13503090.000,y=55594325.000,z=769838.640},
name='Talemai Moon 2',
planetarySystemId=0,
radius=12000
},
[41]={
GM=106830900,
bodyId=41,
center={x=-12800515.000,y=55700259.000,z=325207.840},
name='Talemai Moon 3',
planetarySystemId=0,
radius=11000
},
[42]={
GM=264870000,
bodyId=42,
center={x=-13058408.000,y=55781856.000,z=740177.760},
name='Talemai Moon 1',
planetarySystemId=0,
radius=15000
},
[50]={
GM=499917600,
bodyId=50,
center={x=-43902841.780,y=22261034.700,z=-48862386.000},
name='Feli Moon 1',
planetarySystemId=0,
radius=14000
},
[70]={
GM=396912600,
bodyId=70,
center={x=58969616.000,y=29797945.000,z=57969449.000},
name='Sinnen Moon 1',
planetarySystemId=0,
radius=17000
},
[100]={
GM=13975172474,
bodyId=100,
center={x=98865536.000,y=-13534464.000,z=-934461.990},
name='Lacobus',
planetarySystemId=0,
radius=55650
},
[101]={
GM=264870000,
bodyId=101,
center={x=98905288.170,y=-13950921.100,z=-647589.530},
name='Lacobus Moon 3',
planetarySystemId=0,
radius=15000
},
[102]={
GM=444981600,
bodyId=102,
center={x=99180968.000,y=-13783862.000,z=-926156.400},
name='Lacobus Moon 1',
planetarySystemId=0,
radius=18000
},
[103]={
GM=211503600,
bodyId=103,
center={x=99250052.000,y=-13629215.000,z=-1059341.400},
name='Lacobus Moon 2',
planetarySystemId=0,
radius=14000
},
[110]={
GM=9204742375,
bodyId=110,
center={x=14165536.000,y=-85634465.000,z=-934464.300},
name='Symeon',
planetarySystemId=0,
radius=49050
},
[120]={
GM=7135606629,
bodyId=120,
center={x=2865536.700,y=-99034464.000,z=-934462.020},
name='Ion',
planetarySystemId=0,
radius=44950
},
[121]={
GM=106830900,
bodyId=121,
center={x=2472916.800,y=-99133747.000,z=-1133582.800},
name='Ion Moon 1',
planetarySystemId=0,
radius=11000
},
[122]={
GM=176580000,
bodyId=122,
center={x=2995424.500,y=-99275010.000,z=-1378480.700},
name='Ion Moon 2',
planetarySystemId=0,
radius=15000
}
}
}
end
function PlanetRef()
--[[
Provide coordinate transforms and access to kinematic related parameters
Author: JayleBreak
Usage (unit.start):
PlanetaryReference = require('planetref')
galaxyReference = PlanetaryReference(referenceTableSource)
helios = galaxyReference[0] -- PlanetaryReference.PlanetarySystem instance
alioth = helios[2] -- PlanetaryReference.BodyParameters instance
Methods:
PlanetaryReference:getPlanetarySystem - based on planetary system ID.
PlanetaryReference.isMapPosition - 'true' if an instance of 'MapPosition'
PlanetaryReference.createBodyParameters - for entry into reference table
PlanetaryReference.BodyParameters - a class containing a body's information.
PlanetaryReference.MapPosition - a class for map coordinates
PlanetaryReference.PlanetarySystem - a container for planetary system info.
PlanetarySystem:castIntersections - from a position in a given direction.
PlanetarySystem:closestBody - to the specified coordinates.
PlanetarySystem:convertToBodyIdAndWorldCoordinates - from map coordinates.
PlanetarySystem:getBodyParameters - from reference table.
PlanetarySystem:getPlanetarySystemId - for the instance.
BodyParameters:convertToWorldCoordinates - from map coordinates
BodyParameters:convertToMapPosition - from world coordinates
BodyParameters:getAltitude - of world coordinates
BodyParameters:getDistance - from center to world coordinates
BodyParameters:getGravity - at a given position in world coordinates.
Description
An instance of the 'PlanetaryReference' "class" can contain transform and
kinematic reference information for all planetary systems in DualUniverse.
Each planetary system is identified by a numeric identifier. Currently,
the only planetary system, Helios, has the identifier: zero. This "class"
supports the indexing ('[]') operation which is equivalent to the
use of the 'getPlanetarySystem' method. It also supports the 'pairs()'
method for iterating over planetary systems.
An instance of the 'PlanetarySystem' "class" contains all reference
information for a specific system. It supports the indexing ('[]') and
'pairs()' functions which allows iteration over each "body" in the
system where the key is the numeric body ID. It also supports the
'tostring()' method.
An instance of the 'BodyParameters' "class" contains all reference
information for a single celestial "body" (a moon or planet). It supports
the 'tostring()' method, and contains the data members:
planetarySystemId - numeric planetary system ID
bodyId - numeric body ID
radius - radius of the body in meters (zero altitude)
center - world coordinates of the body's center position
GM - the gravitation parameter (g = GM/radius^2)
Note that the user is allowed to add custom fields (e.g. body name), but
should insure that complex table values have the '__tostring' metamethod
implemented.
Transform and Kinematics:
"World" coordinates is a cartesian coordinate system with an origin at an
arbitrary fixed point in a planetary system and with distances measured in
meters. The coordinates are expressible either as a simple table of 3 values
or an instance of the 'vec3' class. In either case, the planetary system
identity is implicit.
"Map" coordinates is a geographic coordinate system with an origin at the
center of an identified (by a numeric value) celestial body which is a
member of an identified (also a numeric value) planetary system. Note that
the convention that latitude, longitude, and altitude values will be the
position's x, y, and z world coordinates in the special case of body ID 0.
The kinematic parameters in the reference data permit calculations of the
gravitational attraction of the celestial body on other objects.
Reference Data:
This is an example of reference data with a single entry assigned to
planetary system ID 0, and body ID 2 ('Alioth'):
referenceTable = {
[0] = { [2] = { planetarySystemId = 0,
bodyId = 2,
radius = 126068,
center = vec3({x=-8, y=-8, z=-126303}),
GM = 1.572199+11 } -- as in F=-GMm/r^2
}
}
ref=PlanetaryReference(referenceTable)
Collecting Reference Data:
A combination of information from the "Map" screen in the DU user interface,
and values reported by the DU Lua API can be the source of the reference
table's data (planetarySystemId, bodyId, and surfaceArea is from the user
interface):
referenceTable = {}
referenceTable[planetarySystemId][bodyId] =
PlanetaryReference.createBodyParameters(planetarySystemId,
bodyId,
surfaceArea,
core.getConstructWorldPos(),
core.getWorldVertical(),
core.getAltitude(),
core.g())
Adapting Data Sources:
Other sources of data can be adapted or converted. An example of adapting a
table, defined in the file: 'planets.lua', containing information on a single
planetary system and using celestial body name as the key follows (note that
a 'name' field is added to the BodyParameters instance transparently after
construction, and the '__pairs' meta function is required to support the
'closestBody' and '__tostring' methods):
ref=PlanetaryReference(
{[0] = setmetatable(require('planets'),
{ __index = function(bodies, bodyId)
for _,v in pairs(bodies) do
if v and v.bodyId == bodyId then return v end
end
return nil
end,
__pairs = function(bodies)
return function(t, k)
local nk, nv = next(t, k)
if nv then
local GM = nv.gravity * nv.radius^2
local bp = BodyParameters(0,
nv.id,
nv.radius,
nv.pos,
GM)
bp.name = nk
return nk, bp
end
return nk, nv
end, bodies, nil
end })
})
Converting Data Sources:
An instance of 'PlanetaryReference' that has been adapted to a data source
can be used to convert that source to simple table. For example,
using the adapted instance shown above:
load('convertedData=' .. tostring(ref))()
newRef=PlanetaryReference(convertedData)
Also See: kepler.lua
]]--
--[[ START OF LOCAL IMPLEMENTATION DETAILS ]]--
-- Type checks
local function isNumber(n) return type(n) == 'number' end
local function isSNumber(n) return type(tonumber(n)) == 'number' end
local function isTable(t) return type(t) == 'table' end
local function isString(s) return type(s) == 'string' end
local function isVector(v) return isTable(v)
and isNumber(v.x and v.y and v.z) end
local function isMapPosition(m) return isTable(m) and isNumber(m.latitude and
m.longitude and
m.altitude and
m.bodyId and
m.systemId) end
-- Constants
local deg2rad = math.pi/180
local rad2deg = 180/math.pi
local epsilon = 1e-10
local num = ' *([+-]?%d+%.?%d*e?[+-]?%d*)'
local posPattern = '::pos{' .. num .. ',' .. num .. ',' .. num .. ',' ..
num .. ',' .. num .. '}'
-- Utilities
local utils = require('cpml.utils')
local vec3 = require('cpml.vec3')
local clamp = utils.clamp
local function float_eq(a,b)
if a == 0 then return math.abs(b) < 1e-09 end
if b == 0 then return math.abs(a) < 1e-09 end
return math.abs(a - b) < math.max(math.abs(a),math.abs(b))*epsilon
end
local function formatNumber(n)
local result = string.gsub(
string.reverse(string.format('%.4f',n)),
'^0*%.?','')
return result == '' and '0' or string.reverse(result)
end
local function formatValue(obj)
if isVector(obj) then
return string.format('{x=%.3f,y=%.3f,z=%.3f}', obj.x, obj.y, obj.z)
end
if isTable(obj) and not getmetatable(obj) then
local list = {}
local nxt = next(obj)
if type(nxt) == 'nil' or nxt == 1 then -- assume this is an array
list = obj
else
for k,v in pairs(obj) do
local value = formatValue(v)
if type(k) == 'number' then
table.insert(list, string.format('[%s]=%s', k, value))
else
table.insert(list, string.format('%s=%s', k, value))
end
end
end
return string.format('{%s}', table.concat(list, ','))
end
if isString(obj) then
return string.format("'%s'", obj:gsub("'",[[\']]))
end
return tostring(obj)
end
-- CLASSES
-- BodyParameters: Attributes of planetary bodies (planets and moons)
local BodyParameters = {}
BodyParameters.__index = BodyParameters
BodyParameters.__tostring =
function(obj, indent)
local sep = indent or ''
local keys = {}
for k in pairs(obj) do table.insert(keys, k) end
table.sort(keys)
local list = {}
for _, k in ipairs(keys) do
local value = formatValue(obj[k])
if type(k) == 'number' then
table.insert(list, string.format('[%s]=%s', k, value))
else
table.insert(list, string.format('%s=%s', k, value))
end
end
if indent then
return string.format('%s%s',
indent,
table.concat(list, ',\n' .. indent))
end
return string.format('{%s}', table.concat(list, ','))
end
BodyParameters.__eq = function(lhs, rhs)
return lhs.planetarySystemId == rhs.planetarySystemId and
lhs.bodyId == rhs.bodyId and
float_eq(lhs.radius, rhs.radius) and
float_eq(lhs.center.x, rhs.center.x) and
float_eq(lhs.center.y, rhs.center.y) and
float_eq(lhs.center.z, rhs.center.z) and
float_eq(lhs.GM, rhs.GM)
end
local function mkBodyParameters(systemId, bodyId, radius, worldCoordinates, GM)
-- 'worldCoordinates' can be either table or vec3
assert(isSNumber(systemId),
'Argument 1 (planetarySystemId) must be a number:' .. type(systemId))
assert(isSNumber(bodyId),
'Argument 2 (bodyId) must be a number:' .. type(bodyId))
assert(isSNumber(radius),
'Argument 3 (radius) must be a number:' .. type(radius))
assert(isTable(worldCoordinates),
'Argument 4 (worldCoordinates) must be a array or vec3.' ..
type(worldCoordinates))
assert(isSNumber(GM),
'Argument 5 (GM) must be a number:' .. type(GM))
return setmetatable({planetarySystemId = tonumber(systemId),
bodyId = tonumber(bodyId),
radius = tonumber(radius),
center = vec3(worldCoordinates),
GM = tonumber(GM) }, BodyParameters)
end
-- MapPosition: Geographical coordinates of a point on a planetary body.
local MapPosition = {}
MapPosition.__index = MapPosition
MapPosition.__tostring = function(p)
return string.format('::pos{%d,%d,%s,%s,%s}',
p.systemId,
p.bodyId,
formatNumber(p.latitude*rad2deg),
formatNumber(p.longitude*rad2deg),
formatNumber(p.altitude))
end
MapPosition.__eq = function(lhs, rhs)
return lhs.bodyId == rhs.bodyId and
lhs.systemId == rhs.systemId and
float_eq(lhs.latitude, rhs.latitude) and
float_eq(lhs.altitude, rhs.altitude) and
(float_eq(lhs.longitude, rhs.longitude) or
float_eq(lhs.latitude, math.pi/2) or
float_eq(lhs.latitude, -math.pi/2))
end
-- latitude and longitude are in degrees while altitude is in meters
local function mkMapPosition(overload, bodyId, latitude, longitude, altitude)
local systemId = overload -- Id or '::pos{...}' string
if isString(overload) and not longitude and not altitude and
not bodyId and not latitude then
systemId, bodyId, latitude, longitude, altitude =
string.match(overload, posPattern)
assert(systemId, 'Argument 1 (position string) is malformed.')
else
assert(isSNumber(systemId),
'Argument 1 (systemId) must be a number:' .. type(systemId))
assert(isSNumber(bodyId),
'Argument 2 (bodyId) must be a number:' .. type(bodyId))
assert(isSNumber(latitude),
'Argument 3 (latitude) must be in degrees:' .. type(latitude))
assert(isSNumber(longitude),
'Argument 4 (longitude) must be in degrees:' .. type(longitude))
assert(isSNumber(altitude),
'Argument 5 (altitude) must be in meters:' .. type(altitude))
end
systemId = tonumber(systemId)
bodyId = tonumber(bodyId)
latitude = tonumber(latitude)
longitude = tonumber(longitude)
altitude = tonumber(altitude)
if bodyId == 0 then -- this is a hack to represent points in space
return setmetatable({latitude = latitude,
longitude = longitude,
altitude = altitude,
bodyId = bodyId,
systemId = systemId}, MapPosition)
end
return setmetatable({latitude = deg2rad*clamp(latitude, -90, 90),
longitude = deg2rad*(longitude % 360),
altitude = altitude,
bodyId = bodyId,
systemId = systemId}, MapPosition)
end
-- PlanetarySystem - map body IDs to BodyParameters
local PlanetarySystem = {}
PlanetarySystem.__index = PlanetarySystem
PlanetarySystem.__tostring =
function (obj, indent)
local sep = indent and (indent .. ' ' )
local bdylist = {}
local keys = {}
for k in pairs(obj) do table.insert(keys, k) end
table.sort(keys)
for _, bi in ipairs(keys) do
bdy = obj[bi]
local bdys = BodyParameters.__tostring(bdy, sep)
if indent then
table.insert(bdylist,
string.format('[%s]={\n%s\n%s}',
bi, bdys, indent))
else
table.insert(bdylist, string.format(' [%s]=%s', bi, bdys))
end
end
if indent then
return string.format('\n%s%s%s',
indent,
table.concat(bdylist, ',\n' .. indent),
indent)
end
return string.format('{\n%s\n}', table.concat(bdylist, ',\n'))
end
local function mkPlanetarySystem(referenceTable)
local atlas = {}
local pid
for _, v in pairs(referenceTable) do
local id = v.planetarySystemId
if type(id) ~= 'number' then
error('Invalid planetary system ID: ' .. tostring(id))
elseif pid and id ~= pid then
error('Mismatch planetary system IDs: ' .. id .. ' and '
.. pid)
end
local bid = v.bodyId
if type(bid) ~= 'number' then
error('Invalid body ID: ' .. tostring(bid))
elseif atlas[bid] then
error('Duplicate body ID: ' .. tostring(bid))
end
setmetatable(v.center, getmetatable(vec3.unit_x))
atlas[bid] = setmetatable(v, BodyParameters)
pid = id
end
return setmetatable(atlas, PlanetarySystem)
end
-- PlanetaryReference - map planetary system ID to PlanetarySystem
PlanetaryReference = {}
local function mkPlanetaryReference(referenceTable)
return setmetatable({ galaxyAtlas = referenceTable or {} },
PlanetaryReference)
end
PlanetaryReference.__index =
function(t,i)
if type(i) == 'number' then
local system = t.galaxyAtlas[i]
return mkPlanetarySystem(system)
end
return rawget(PlanetaryReference, i)
end
PlanetaryReference.__pairs =
function(obj)
return function(t, k)
local nk, nv = next(t, k)
return nk, nv and mkPlanetarySystem(nv)
end, obj.galaxyAtlas, nil
end
PlanetaryReference.__tostring =
function (obj)
local pslist = {}
for _,ps in pairs(obj or {}) do
local psi = ps:getPlanetarySystemId()
local pss = PlanetarySystem.__tostring(ps, ' ')
table.insert(pslist,
string.format(' [%s]={%s\n }', psi, pss))
end
return string.format('{\n%s\n}\n', table.concat(pslist,',\n'))
end
--[[ START OF PUBLIC INTERFACE ]]--
-- PlanetaryReference CLASS METHODS:
--
-- BodyParameters - create an instance of BodyParameters class
-- planetarySystemId [in]: the body's planetary system ID.
-- bodyId [in]: the body's ID.
-- radius [in]: the radius in meters of the planetary body.
-- bodyCenter [in]: the world coordinates of the center (vec3 or table).
-- GM [in]: the body's standard gravitational parameter.
-- return: an instance of BodyParameters class.
--
PlanetaryReference.BodyParameters = mkBodyParameters
--
-- MapPosition - create an instance of the MapPosition class
-- overload [in]: either a planetary system ID or a position string ('::pos...')
-- bodyId [in]: (ignored if overload is a position string) the body's ID.
-- latitude [in]: (ignored if overload is a position string) the latitude.
-- longitude [in]:(ignored if overload is a position string) the longitude.
-- altitude [in]: (ignored if overload is a position string) the altitude.
-- return: the class instance
--
PlanetaryReference.MapPosition = mkMapPosition
--
-- PlanetarySystem - create an instance of PlanetarySystem class
-- referenceData [in]: a table (indexed by bodyId) of body reference info.
-- return: the class instance
--
PlanetaryReference.PlanetarySystem = mkPlanetarySystem
--
-- createBodyParameters - create an instance of BodyParameters class
-- planetarySystemId [in]: the body's planetary system ID.
-- bodyId [in]: the body's ID.
-- surfaceArea [in]: the body's surface area in square meters.
-- aPosition [in]: world coordinates of a position near the body.
-- verticalAtPosition [in]: a vector pointing towards the body center.
-- altitudeAtPosition [in]: the altitude in meters at the position.
-- gravityAtPosition [in]: the magnitude of the gravitational acceleration.
-- return: an instance of BodyParameters class.
--
function PlanetaryReference.createBodyParameters(planetarySystemId,
bodyId,
surfaceArea,
aPosition,
verticalAtPosition,
altitudeAtPosition,
gravityAtPosition)
assert(isSNumber(planetarySystemId),
'Argument 1 (planetarySystemId) must be a number:' ..
type(planetarySystemId))
assert(isSNumber(bodyId),
'Argument 2 (bodyId) must be a number:' .. type(bodyId))
assert(isSNumber(surfaceArea),
'Argument 3 (surfaceArea) must be a number:' .. type(surfaceArea))
assert(isTable(aPosition),
'Argument 4 (aPosition) must be an array or vec3:' ..
type(aPosition))
assert(isTable(verticalAtPosition),
'Argument 5 (verticalAtPosition) must be an array or vec3:' ..
type(verticalAtPosition))
assert(isSNumber(altitudeAtPosition),
'Argument 6 (altitude) must be in meters:' ..
type(altitudeAtPosition))
assert(isSNumber(gravityAtPosition),
'Argument 7 (gravityAtPosition) must be number:' ..
type(gravityAtPosition))
local radius = math.sqrt(surfaceArea/4/math.pi)
local distance = radius + altitudeAtPosition
local center = vec3(aPosition) + distance*vec3(verticalAtPosition)
local GM = gravityAtPosition * distance * distance
return mkBodyParameters(planetarySystemId, bodyId, radius, center, GM)
end
--
-- isMapPosition - check for the presence of the 'MapPosition' fields
-- valueToTest [in]: the value to be checked
-- return: 'true' if all required fields are present in the input value
--
PlanetaryReference.isMapPosition = isMapPosition
-- PlanetaryReference INSTANCE METHODS:
--
-- getPlanetarySystem - get the planetary system using ID or MapPosition as key
-- overload [in]: either the planetary system ID or a MapPosition that has it.
-- return: instance of 'PlanetarySystem' class or nil on error
--
function PlanetaryReference:getPlanetarySystem(overload)
--if galaxyAtlas then
local planetarySystemId = overload
if isMapPosition(overload) then
planetarySystemId = overload.systemId
end
if type(planetarySystemId) == 'number' then
local system = self.galaxyAtlas[i]
if system then
if getmetatable(nv) ~= PlanetarySystem then
system = mkPlanetarySystem(system)
end
return system
end
end
--end
--return nil
end
-- PlanetarySystem INSTANCE METHODS:
--
-- castIntersections - Find the closest body that intersects a "ray cast".
-- origin [in]: the origin of the "ray cast" in world coordinates
-- direction [in]: the direction of the "ray cast" as a 'vec3' instance.
-- sizeCalculator [in]: (default: returns 1.05*radius) Returns size given body.
-- bodyIds[in]: (default: all IDs in system) check only the given IDs.
-- return: The closest body that blocks the cast or 'nil' if none.
--
function PlanetarySystem:castIntersections(origin,
direction,
sizeCalculator,
bodyIds)
local sizeCalculator = sizeCalculator or
function (body) return 1.05*body.radius end
local candidates = {}
if bodyIds then
for _,i in ipairs(bodyIds) do candidates[i] = self[i] end
else
bodyIds = {}
for k,body in pairs(self) do
table.insert(bodyIds, k)
candidates[k] = body
end
end
local function compare(b1,b2)
local v1 = candidates[b1].center - origin
local v2 = candidates[b2].center - origin
return v1:len() < v2:len()
end
table.sort(bodyIds, compare)
local dir = direction:normalize()
for i, id in ipairs(bodyIds) do
local body = candidates[id]
local c_oV3 = body.center - origin
local radius = sizeCalculator(body)
local dot = c_oV3:dot(dir)
local desc = dot^2 - (c_oV3:len2() - radius^2)
if desc >= 0 then
local root = math.sqrt(desc)
local farSide = dot + root
local nearSide = dot - root
if nearSide > 0 then
return body, farSide, nearSide
elseif farSide > 0 then
return body, farSide, nil
end
end
end
return nil, nil, nil
end
--
-- closestBody - find the closest body to a given set of world coordinates
-- coordinates [in]: the world coordinates of position in space
-- return: an instance of the BodyParameters object closest to 'coordinates'
--
function PlanetarySystem:closestBody(coordinates)
assert(type(coordinates) == 'table', 'Invalid coordinates.')
local minDistance2, body
local coord = vec3(coordinates)
for _,params in pairs(self) do
local distance2 = (params.center - coord):len2()
if not body or distance2 < minDistance2 then
body = params
minDistance2 = distance2
end
end
return body
end
--
-- convertToBodyIdAndWorldCoordinates - map to body Id and world coordinates
-- overload [in]: an instance of MapPosition or a position string ('::pos...)
-- return: a vec3 instance containing the world coordinates or 'nil' on error.
--
function PlanetarySystem:convertToBodyIdAndWorldCoordinates(overload)
local mapPosition = overload
if isString(overload) then
mapPosition = mkMapPosition(overload)
end
if mapPosition.bodyId == 0 then
return 0, vec3(mapPosition.latitude,
mapPosition.longitude,
mapPosition.altitude)
end
local params = self:getBodyParameters(mapPosition)
if params then
return mapPosition.bodyId,
params:convertToWorldCoordinates(mapPosition)
end
end
--
-- getBodyParameters - get or create an instance of BodyParameters class
-- overload [in]: either an instance of MapPosition or a body's ID.
-- return: a BodyParameters instance or 'nil' if body ID is not found.
--
function PlanetarySystem:getBodyParameters(overload)
local bodyId = overload
if isMapPosition(overload) then
bodyId = overload.bodyId
end
assert(isSNumber(bodyId),
'Argument 1 (bodyId) must be a number:' .. type(bodyId))
return self[bodyId]
end
--
-- getPlanetarySystemId - get the planetary system ID for this instance
-- return: the planetary system ID or nil if no planets are in the system.
--
function PlanetarySystem:getPlanetarySystemId()
local k, v = next(self)
return v and v.planetarySystemId
end
-- BodyParameters INSTANCE METHODS:
--
-- convertToMapPosition - create an instance of MapPosition from coordinates
-- worldCoordinates [in]: the world coordinates of the map position.
-- return: an instance of MapPosition class
--
function BodyParameters:convertToMapPosition(worldCoordinates)
assert(isTable(worldCoordinates),
'Argument 1 (worldCoordinates) must be an array or vec3:' ..
type(worldCoordinates))
local worldVec = vec3(worldCoordinates)
if self.bodyId == 0 then
return setmetatable({latitude = worldVec.x,
longitude = worldVec.y,
altitude = worldVec.z,
bodyId = 0,
systemId = self.planetarySystemId}, MapPosition)
end
local coords = worldVec - self.center
local distance = coords:len()
local altitude = distance - self.radius
local latitude = 0
local longitude = 0
if not float_eq(distance, 0) then
local phi = math.atan(coords.y, coords.x)
longitude = phi >= 0 and phi or (2*math.pi + phi)
latitude = math.pi/2 - math.acos(coords.z/distance)
end
return setmetatable({latitude = latitude,
longitude = longitude,
altitude = altitude,
bodyId = self.bodyId,
systemId = self.planetarySystemId}, MapPosition)
end
--
-- convertToWorldCoordinates - convert a map position to world coordinates
-- overload [in]: an instance of MapPosition or a position string ('::pos...')
--
function BodyParameters:convertToWorldCoordinates(overload)
local mapPosition = isString(overload) and
mkMapPosition(overload) or overload
if mapPosition.bodyId == 0 then -- support deep space map position
return vec3(mapPosition.latitude,
mapPosition.longitude,
mapPosition.altitude)
end
assert(isMapPosition(mapPosition),
'Argument 1 (mapPosition) is not an instance of "MapPosition".')
assert(mapPosition.systemId == self.planetarySystemId,
'Argument 1 (mapPosition) has a different planetary system ID.')
assert(mapPosition.bodyId == self.bodyId,
'Argument 1 (mapPosition) has a different planetary body ID.')
local xproj = math.cos(mapPosition.latitude)
return self.center + (self.radius + mapPosition.altitude) *
vec3(xproj*math.cos(mapPosition.longitude),
xproj*math.sin(mapPosition.longitude),
math.sin(mapPosition.latitude))
end
--
-- getAltitude - calculate the altitude of a point given in world coordinates.
-- worldCoordinates [in]: the world coordinates of the point.
-- return: the altitude in meters
--
function BodyParameters:getAltitude(worldCoordinates)
return (vec3(worldCoordinates) - self.center):len() - self.radius
end
--
-- getDistance - calculate the distance to a point given in world coordinates.
-- worldCoordinates [in]: the world coordinates of the point.
-- return: the distance in meters
--
function BodyParameters:getDistance(worldCoordinates)
return (vec3(worldCoordinates) - self.center):len()
end
--
-- getGravity - calculate the gravity vector induced by the body.
-- worldCoordinates [in]: the world coordinates of the point.
-- return: the gravity vector in meter/seconds^2
--
function BodyParameters:getGravity(worldCoordinates)
local radial = self.center - vec3(worldCoordinates) -- directed towards body
local len2 = radial:len2()
return (self.GM/len2) * radial/math.sqrt(len2)
end
-- end of module
return setmetatable(PlanetaryReference,
{ __call = function(_,...)
return mkPlanetaryReference(...)
end })
end
function Keplers()
--[[
Provides methods for computing orbital information for an object
Usage:
Kepler = require('autoconf.custom.kepler')
alioth = Kepler({ GM=157470826617,
bodyId=2,
center={x=-8.000,y=-8.000,z=-126303.000},
name='Alioth',
planetarySystemId=0,
radius=126068
})
altitude = 6000
position = '::pos{0,2,0,0,6000}'
e, o = alioth:escapeAndOrbitalSpeed(altitude)
orbit = alioth:orbitalParameters(position, {0, o+1, 0})
print("Eccentricity " .. orbit.eccentricity)
print("Perihelion " .. orbit.periapsis.altitude)
print("Max. speed " .. orbit.periapsis.speed)
print("Circular orbit speed " .. orbit.periapsis.circularOrbitSpeed)
print("Aphelion " .. orbit.apoapsis.altitude)
print("Min. speed " .. orbit.apoapsis.speed)
print("Orbital period " .. orbit.period)
--- output:
Eccentricity 0.0018324307017878
Perihelion 6000.0
Max. speed 1092.9462297033
Circular orbit speed 1091.9462297033
Aphelion 6484.8994605062
Min. speed 1088.9480596194
Orbital period 762.02818214049
Methods:
Kepler:escapeAndOrbitalSpeed - for a given celestial body and altitude.
Kepler:orbitalParameters - for a given massless object and a celestial body.
Description
The motion of an object in the vicinity of substantially larger mass is
in the domain of the "2-body problem". By assuming the object whose motion
is of interest is of negligable mass simplifies the calculations of:
the speed to escape the body, the speed of a circular orbit, and the
parameters defining the orbit of the object (or the lack of orbit as the
case may be).
Orbital Parameters:
periapsis - the closest approach to the planet
apoapsis - the furthest point from the planet if in orbit (otherwise nil)
eccentricity - 0 for circular orbits
<1 for elliptical orbits
1 for parabiolic trajectory
>1 for hyperbolic trajectory
period - time (in seconds) to complete an orbit
Also See: planetref.lua
]]--
local vec3 = require('cpml.vec3')
local PlanetRef = PlanetRef()
local function isString(s) return type(s) == 'string' end
local function isTable(t) return type(t) == 'table' end
local function float_eq(a,b)
if a == 0 then return math.abs(b) < 1e-09 end
if b == 0 then return math.abs(a) < 1e-09 end
return math.abs(a - b) < math.max(math.abs(a),math.abs(b))*epsilon
end
Kepler = {}
Kepler.__index = Kepler
--
-- escapeAndOrbitalSpeed - speed required to escape and for a circular orbit
-- altitude [in]: the height of the orbit in meters above "sea-level"
-- return: the speed in m/s needed to escape the celestial body and to orbit it.
--
function Kepler:escapeAndOrbitalSpeed(altitude)
assert(self.body)
-- P = -GMm/r and KE = mv^2/2 (no lorentz factor used)
-- mv^2/2 = GMm/r
-- v^2 = 2GM/r
-- v = sqrt(2GM/r1)
local distance = altitude + self.body.radius
if not float_eq(distance, 0) then
local orbit = math.sqrt(self.body.GM/distance)
return math.sqrt(2)*orbit, orbit
end
return nil, nil
end
--
-- orbitalParameters: determine the orbital elements for a two-body system.
-- overload [in]: the world coordinates or map coordinates of a massless object.
-- velocity [in]: The velocity of the massless point object in m/s.
-- return: the 6 orbital elements for the massless object.
--
function Kepler:orbitalParameters(overload, velocity)
assert(self.body)
assert(isTable(overload) or isString(overload))
assert(isTable(velocity))
local pos = (isString(overload) or PlanetRef.isMapPosition(overload)) and
self.body:convertToWorldCoordinates(overload) or
vec3(overload)
local v = vec3(velocity)
local r = pos - self.body.center
local v2 = v:len2()
local d = r:len()
local mu = self.body.GM
local e = ((v2 - mu/d)*r - r:dot(v)*v)/mu
local a = mu/(2*mu/d - v2)
local ecc = e:len()
local dir = e:normalize()
local pd = a*(1-ecc)
local ad = a*(1+ecc)
local per = pd*dir + self.body.center
local apo = ecc <= 1 and -ad*dir + self.body.center or nil
local trm = math.sqrt(a*mu*(1-ecc*ecc))
local Period = apo and 2*math.pi*math.sqrt(a^3/mu)
-- These are great and all, but, I need more.
local trueAnomaly = math.acos((e:dot(r))/(ecc*d))
if r:dot(v) < 0 then
trueAnomaly = -(trueAnomaly - 2*math.pi)
end
-- Apparently... cos(EccentricAnomaly) = (cos(trueAnomaly) + eccentricity)/(1 + eccentricity * cos(trueAnomaly))
local EccentricAnomaly = math.acos((math.cos(trueAnomaly) + ecc)/(1 + ecc * math.cos(trueAnomaly)))
-- Then.... apparently if this is below 0, we should add 2pi to it
-- I think also if it's below 0, we're past the apoapsis?
local timeTau = EccentricAnomaly
if timeTau < 0 then
timeTau = timeTau + 2*math.pi
end
-- So... time since periapsis...
-- Is apparently easy if you get mean anomly. t = M/n where n is mean motion, = 2*pi/Period
local MeanAnomaly = timeTau - ecc * math.sin(timeTau)
local TimeSincePeriapsis = MeanAnomaly/(2*math.pi/Period)
--system.print(MeanAnomaly .. " - " .. TimeSincePeriapsis .. " - " .. Period .. " - " .. EccentricAnomaly .. " - " .. timeTau .. " - " .. trueAnomaly)
-- Mean anom is 0 at periapsis, positive before it... and positive after it.
-- I guess this is why I needed to use timeTau and not EccentricAnomaly here
local TimeToPeriapsis = Period - TimeSincePeriapsis
local TimeToApoapsis = TimeToPeriapsis + Period/2
if trueAnomaly - math.pi > 0 then -- TBH I think something's wrong in my formulas because I needed this.
TimeToPeriapsis = TimeSincePeriapsis
TimeToApoapsis = TimeToPeriapsis + Period/2
end
if TimeToApoapsis > Period then
TimeToApoapsis = TimeToApoapsis - Period
end
return { periapsis = { position = per,
speed = trm/pd,
circularOrbitSpeed = math.sqrt(mu/pd),
altitude = pd - self.body.radius},
apoapsis = apo and
{ position = apo,
speed = trm/ad,
circularOrbitSpeed = math.sqrt(mu/ad),
altitude = ad - self.body.radius},
currentVelocity = v,
currentPosition = pos,
eccentricity = ecc,
period = Period,
eccentricAnomaly = EccentricAnomaly,
meanAnomaly = MeanAnomaly,
timeToPeriapsis = TimeToPeriapsis,
timeToApoapsis = TimeToApoapsis
}
end
local function new(bodyParameters)
local params = PlanetRef.BodyParameters(bodyParameters.planetarySystemId,
bodyParameters.bodyId,
bodyParameters.radius,
bodyParameters.center,
bodyParameters.GM)
return setmetatable({body = params}, Kepler)
end
return setmetatable(Kepler, { __call = function(_,...) return new(...) end })
end
function Kinematics()
--[[
DualUniverse kinematic equations
Author: JayleBreak
Usage (unit.start):
Kinematics = require('autoconf.custom.kinematics')
Methods:
computeAccelerationTime - "relativistic" version of t = (vf - vi)/a
computeDistanceAndTime - Return distance & time needed to reach final speed.
computeTravelTime - "relativistic" version of t=(sqrt(2ad+v^2)-v)/a
Description
DualUniverse increases the effective mass of constructs as their absolute
speed increases by using the "lorentz" factor (from relativity) as the scale
factor. This results in an upper bound on the absolute speed of constructs
(excluding "warp" drive) that is set to 30 000 KPH (8 333 MPS). This module
provides utilities for computing some physical quantities taking this
scaling into account.
]]--
local Kinematic = {} -- just a namespace
local C = 30000000/3600
local C2 = C*C
local ITERATIONS = 100 -- iterations over engine "warm-up" period
local function lorentz(v) return 1/math.sqrt(1 - v*v/C2) end
--
-- computeAccelerationTime - "relativistic" version of t = (vf - vi)/a
-- initial [in]: initial (positive) speed in meters per second.
-- acceleration [in]: constant acceleration until 'finalSpeed' is reached.
-- final [in]: the speed at the end of the time interval.
-- return: the time in seconds spent in traversing the distance
--
function Kinematic.computeAccelerationTime(initial, acceleration, final)
-- The low speed limit of following is: t=(vf-vi)/a (from: vf=vi+at)
local k1 = C*math.asin(initial/C)
return (C * math.asin(final/C) - k1)/acceleration
end
--
-- computeDistanceAndTime - Return distance & time needed to reach final speed.
-- initial[in]: Initial speed in meters per second.
-- final[in]: Final speed in meters per second.
-- restMass[in]: Mass of the construct at rest in Kg.
-- thrust[in]: Engine's maximum thrust in Newtons.
-- t50[in]: (default: 0) Time interval to reach 50% thrust in seconds.
-- brakeThrust[in]: (default: 0) Constant thrust term when braking.
-- return: Distance (in meters), time (in seconds) required for change.
--
function Kinematic.computeDistanceAndTime(initial,
final,
restMass,
thrust,
t50,
brakeThrust)
-- This function assumes that the applied thrust is colinear with the
-- velocity. Furthermore, it does not take into account the influence
-- of gravity, not just in terms of its impact on velocity, but also
-- its impact on the orientation of thrust relative to velocity.
-- These factors will introduce (usually) small errors which grow as
-- the length of the trip increases.
t50 = t50 or 0
brakeThrust = brakeThrust or 0 -- usually zero when accelerating
local tau0 = lorentz(initial)
local speedUp = initial <= final
local a0 = thrust * (speedUp and 1 or -1)/restMass
local b0 = -brakeThrust/restMass
local totA = a0+b0
if speedUp and totA <= 0 or not speedUp and totA >= 0 then
return -1, -1 -- no solution
end
local distanceToMax, timeToMax = 0, 0
-- If, the T50 time is set, then assume engine is at zero thrust and will
-- reach full thrust in 2*T50 seconds. Thrust curve is given by:
-- Thrust: F(z)=(a0*(1+sin(z))+2*b0)/2 where z=pi*(t/t50 - 1)/2
-- Acceleration is given by F(z)/m(z) where m(z) = m/sqrt(1-v^2/c^2)
-- or v(z)' = (a0*(1+sin(z))+2*b0)*sqrt(1-v(z)^2/c^2)/2
if a0 ~= 0 and t50 > 0 then
-- Closed form solution for velocity exists:
-- v(t) = -c*tan(w)/sqrt(tan(w)^2+1) => w = -asin(v/c)
-- w=(pi*t*(a0/2+b0)-a0*t50*sin(pi*t/2/t50)+*pi*c*k1)/pi/c
-- @ t=0, v(0) = vi
-- pi*c*k1/pi/c = -asin(vi/c)
-- k1 = asin(vi/c)
local k1 = math.asin(initial/C)
local c1 = math.pi*(a0/2+b0)
local c2 = a0*t50
local c3 = C*math.pi
local v = function(t)
local w = (c1*t - c2*math.sin(math.pi*t/2/t50) + c3*k1)/c3
local tan = math.tan(w)
return C*tan/math.sqrt(tan*tan+1)
end
local speedchk = speedUp and function(s) return s >= final end or
function(s) return s <= final end
timeToMax = 2*t50
if speedchk(v(timeToMax)) then
local lasttime = 0
while math.abs(timeToMax - lasttime) > 0.5 do
local t = (timeToMax + lasttime)/2
if speedchk(v(t)) then
timeToMax = t
else
lasttime = t
end
end
end
-- There is no closed form solution for distance in this case.
-- Numerically integrate for time t=0 to t=2*T50 (or less)
local lastv = initial
local tinc = timeToMax/ITERATIONS
for step = 1, ITERATIONS do
local speed = v(step*tinc)
distanceToMax = distanceToMax + (speed+lastv)*tinc/2
lastv = speed
end
if timeToMax < 2*t50 then
return distanceToMax, timeToMax
end
initial = lastv
end
-- At full thrust, acceleration only depends on the Lorentz factor:
-- v(t)' = (F/m(v)) = a*sqrt(1-v(t)^2/c^2) where a = a0+b0
-- -> v = c*sin((at+k1)/c)
-- @ t=0, v=vi: k1 = c*asin(vi/c)
-- -> t = (c*asin(v/c) - k1)/a
-- x(t)' = c*sin((at+k1)/c)
-- x = k2 - c^2 cos((at+k1)/c)/a
-- @ t=0, x=0: k2 = c^2 * cos(k1/c)/a
local k1 = C*math.asin(initial/C)
local time = (C * math.asin(final/C) - k1)/totA
local k2 = C2 *math.cos(k1/C)/totA
local distance = k2 - C2 * math.cos((totA*time + k1)/C)/totA
return distance+distanceToMax, time+timeToMax
end
--
-- computeTravelTime - "relativistic" version of t=(sqrt(2ad+v^2)-v)/a
-- initialSpeed [in]: initial (positive) speed in meters per second
-- acceleration [in]: constant acceleration until 'distance' is traversed
-- distance [in]: the distance traveled in meters
-- return: the time in seconds spent in traversing the distance
--
function Kinematic.computeTravelTime(initial, acceleration, distance)
-- The low speed limit of following is: t=(sqrt(2ad+v^2)-v)/a
-- (from: d=vt+at^2/2)
if distance == 0 then return 0 end
if acceleration > 0 then
local k1 = C*math.asin(initial/C)
local k2 = C2*math.cos(k1/C)/acceleration
return (C*math.acos(acceleration*(k2 - distance)/C2) - k1)/acceleration
end
assert(initial > 0, 'Acceleration and initial speed are both zero.')
return distance/initial
end
function Kinematic.lorentz(v) return lorentz(v) end
return Kinematic
end
PlanetaryReference = PlanetRef()
galaxyReference = PlanetaryReference(Atlas())
Kinematic = Kinematics()
Kep = Keplers()
function getDistanceDisplayString(distance)
local su = distance > 100000
local result = ""
if su then
-- Convert to SU
result = round(distance/1000/200,1) .. " SU"
else
-- Convert to KM
result = round(distance/1000,1) .. " KM"
end
return result
end
PlanetaryReference = PlanetRef()
galaxyReference = PlanetaryReference(Atlas())
MapScreenButtons = {}
MapScreenMouseX = 0
MapScreenMouseY = 0
MapScreenMouseDown = false
MapScreenButtonSelected = 0
local worldPos = vec3(core.getConstructWorldPos())
local locX = (worldPos.x/400000)
local locY = (worldPos.y/400000)*(-1)
local destX = 0
local destY = 0
local sudistance = 0
local loc = vec3(core.getConstructWorldPos())
local ion = galaxyReference[0][120] ---uses Atlas functions
local thades = vec3(29165536.000, 10865536.000, 65536.000)
local sinnen = vec3(58665536.000, 29665536.000, 58165536.000)
local alioth = galaxyReference[0][2] ---uses Atlas functions
local madis = vec3(17465536.000, 22665536.000, -34464.000)
local jago = vec3(-94134464.000, 12765536.000, -3634464.000)
local symeon = vec3(14165536.000, -85634464.000, -934464.000)
local lacobus = vec3(98865536.000, -13534464.000, -934464.000)
local teoma = vec3(80865536.000, 54665536.000, -934464.000)
local feli = vec3(-43534464.000, 22565536.000, -48934464.000)
local talemai = vec3(-13234464.000, 55765536.000, 465536.000)
local sicari = vec3(52765536.000, 27165536.000, 52065536.000)
local distion = math.floor(ion:getDistance(loc)/200000) ---uses getDistance functions----
local distthades = string.format("%.2f", math.sqrt((loc.x-thades.x)^2+(loc.y-thades.y)^2+(loc.z-thades.z)^2)/200000)
local distalioth = math.floor(alioth:getDistance(loc)/200000) ---uses getDistance functions----
local distmadis = string.format("%.2f", math.sqrt((loc.x-madis.x)^2+(loc.y-madis.y)^2+(loc.z-madis.z)^2)/200000)
local distjago = string.format("%.2f", math.sqrt((loc.x-jago.x)^2+(loc.y-jago.y)^2+(loc.z-jago.z)^2)/200000)
local distlacobus = string.format("%.2f", math.sqrt((loc.x-lacobus.x)^2+(loc.y-lacobus.y)^2+(loc.z-lacobus.z)^2)/200000)
local distteoma = string.format("%.2f", math.sqrt((loc.x-teoma.x)^2+(loc.y-teoma.y)^2+(loc.z-teoma.z)^2)/200000)
local distsymeon = string.format("%.2f", math.sqrt((loc.x-symeon.x)^2+(loc.y-symeon.y)^2+(loc.z-symeon.z)^2)/200000)
local distfeli = string.format("%.2f", math.sqrt((loc.x-feli.x)^2+(loc.y-feli.y)^2+(loc.z-feli.z)^2)/200000)
local distsinnen = string.format("%.2f", math.sqrt((loc.x-sinnen.x)^2+(loc.y-sinnen.y)^2+(loc.z-sinnen.z)^2)/200000)
local disttalemai = string.format("%.2f", math.sqrt((loc.x-talemai.x)^2+(loc.y-talemai.y)^2+(loc.z-talemai.z)^2)/200000)
local distsicari = string.format("%.2f", math.sqrt((loc.x-sicari.x)^2+(loc.y-sicari.y)^2+(loc.z-sicari.z)^2)/200000)
for i = 1,1 do
local button = {id = ("b"..1), enabled=true, td="<td>", top=2/100, bottom=13/100, left=1/100, right=28/100}
table.insert(MapScreenButtons, button)
end
for i = 2,2 do
local button = {id = ("b"..2), enabled=true, td="<td>", top=15/100, bottom=26/100, left=1/100, right=30/100}
table.insert(MapScreenButtons, button)
end
for i = 3,3 do
local button = {id = ("b"..3), enabled=true, td="<td>", top=27/100, bottom=38/100, left=1/100, right=28/100}
table.insert(MapScreenButtons, button)
end
for i = 4,4 do
local button = {id = ("b"..4), enabled=true, td="<td>", top=39/100, bottom=50/100, left=1/100, right=28/100}
table.insert(MapScreenButtons, button)
end
for i = 5,5 do
local button = {id = ("b"..5), enabled=true, td="<td>", top=51/100, bottom=62/100, left=1/100, right=28/100}
table.insert(MapScreenButtons, button)
end
for i = 6,6 do
local button = {id = ("b"..6), enabled=true, td="<td>", top=64/100, bottom=75/100, left=1/100, right=28/100}
table.insert(MapScreenButtons, button)
end
for i = 7,7 do
local button = {id = ("b"..7), enabled=true, td="<td>", top=2/100, bottom=13/100, left=75/100, right=100/100}
table.insert(MapScreenButtons, button)
end
for i = 8,8 do
local button = {id = ("b"..8), enabled=true, td="<td>", top=15/100, bottom=26/100, left=75/100, right=100/100}
table.insert(MapScreenButtons, button)
end
for i = 9,9 do
local button = {id = ("b"..9), enabled=true, td="<td>", top=27/100, bottom=38/100, left=75/100, right=100/100}
table.insert(MapScreenButtons, button)
end
for i = 10,10 do
local button = {id = ("b"..10), enabled=true, td="<td>", top=39/100, bottom=50/100, left=75/100, right=100/100}
table.insert(MapScreenButtons, button)
end
for i = 11,11 do
local button = {id = ("b"..11), enabled=true, td="<td>", top=51/100, bottom=62/100, left=75/100, right=100/100}
table.insert(MapScreenButtons, button)
end
for i = 12,12 do
local button = {id = ("b"..12), enabled=true, td="<td>", top=64/100, bottom=75/100, left=75/100, right=100/100}
table.insert(MapScreenButtons, button)
end
for i = 13,13 do
local button = {id = ("b"..13), enabled=true, td="<td>", top=90/100, bottom=100/100, left=1/100, right=18/100}
table.insert(MapScreenButtons, button)
end
function evaluateButtons()
local selected = 0
if #MapScreenButtons >= 1 then
-- Set button styles
for i, button in ipairs(MapScreenButtons) do
if button.left < MapScreenMouseX and MapScreenMouseX < button.right and button.top < MapScreenMouseY and MapScreenMouseY < button.bottom then
if MapScreenMouseDown and MapScreenButtonSelected == i then
end
selected = i
end
if not button.enabled then
end
end
end
return selected
end
function onButtonDown(buttonNo)
local button = MapScreenButtons[buttonNo]
if not button or not button.enabled then
return
end
end
function onButtonUp(buttonNo)
local button = MapScreenButtons[buttonNo]
if not button or not button.enabled then
return
end
function onClick(buttonNo)
local button = MapScreenButtons[buttonNo]
if not button or not button.enabled then
return
end
end
if buttonNo == 1 then
destX = 0
destY = 0
sudistance = distalioth
elseif buttonNo == 2 then
destX = 43
destY = -56
sudistance = distmadis
elseif buttonNo == 3 then
destX = 73
destY = -27
sudistance = distthades
elseif buttonNo == 4 then
destX = -33
destY = -139
sudistance = disttalemai
elseif buttonNo == 5 then
destX = -109
destY = -56
sudistance = distfeli
elseif buttonNo == 6 then
destX = 131
destY = -68
sudistance = distsicari
elseif buttonNo == 7 then
destX = 35
destY = 214
sudistance = distsymeon
elseif buttonNo == 8 then
destX = 146
destY = -74
sudistance = distsinnen
elseif buttonNo == 9 then
destX = -235
destY = -32
sudistance = distjago
elseif buttonNo == 10 then
destX = 202
destY = -137
sudistance = distteoma
elseif buttonNo == 11 then
destX = 7
destY = 247
sudistance = distion
elseif buttonNo == 12 then
destX = 247
destY = 34
sudistance = distlacobus
elseif buttonNo == 13 then
unit.exit()
end
end
function updateScreen()
warpmath = math.floor(math.floor(core.getConstructMass()/ 1000) * sudistance * 0.00025)
html= ([[
<svg class="bootstrap" viewBox="0 0 1024 1024" style="width:100%; height:100%"><circle cx="500" cy="500" r="400" stroke="darkgreen" stroke-width="3" transform=""></circle><circle cx="500" cy="500" r="350" stroke="darkgreen" stroke-width="3" transform="" stroke-opacity="0.2"></circle><circle cx="500" cy="500" r="300" stroke="darkgreen" stroke-width="3" transform=""></circle><circle cx="500" cy="500" r="250" stroke="darkgreen" stroke-width="3" transform="" stroke-opacity="0.2"></circle><circle cx="500" cy="500" r="200" stroke="darkgreen" stroke-width="3" transform=""></circle><circle cx="500" cy="500" r="150" stroke="darkgreen" stroke-width="3" transform="" stroke-opacity="0.2"></circle><circle cx="500" cy="500" r="100" stroke="lightblue" stroke-width="3" transform=""></circle><circle cx="500" cy="500" r="50" stroke="lightblue" stroke-width="3" transform="" stroke-opacity="0.2"></circle><circle cx="500" cy="500" r="20" stroke="Orange" stroke-width="2" transform=""></circle><text x="510" y="510" fill="Yellow">Helios</text><circle cx="-0.00" cy="0" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="-0.00" y="0" transform="translate(500,480)" fill="white" font-size="20">Alioth</text><circle cx="7.16" cy="247.59" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="7.16" y="247.59" transform="translate(480,480)" fill="white" font-size="20">Ion</text><circle cx="35.41" cy="214.09" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="35.41" y="214.09" transform="translate(500,480)" fill="white" font-size="20">Symeon</text><circle cx="-33.09" cy="-139.41" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="-33.09" y="-139.41" transform="translate(500,480)" fill="white" font-size="20">Talemai</text><circle cx="202.16" cy="-136.66" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="202.16" y="-136.66" transform="translate(500,480)" fill="white" font-size="20">Teoma</text><circle cx="247.16" cy="33.84" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="247.16" y="33.84" transform="translate(500,480)" fill="white" font-size="20">Lacobus</text><circle cx="-108.84" cy="-56.41" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="-108.84" y="-56.41" transform="translate(500,480)" fill="white" font-size="20">Feli</text><circle cx="72.91" cy="-27.16" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="72.91" y="-27.16" transform="translate(500,485)" fill="white" font-size="20">Thades</text><circle cx="43.66" cy="-56.66" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="43.66" y="-56.66" transform="translate(500,480)" fill="white" font-size="20">Madis</text><circle cx="-235.34" cy="-31.91" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="-235.34" y="-31.91" transform="translate(500,480)" fill="white" font-size="20">Jago</text><circle cx="131.91" cy="-67.91" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="131.91" y="-67.91" transform="translate(475,480)" fill="white" font-size="20">Sicari</text><circle cx="146.66" cy="-74.16" r="10" stroke="black" stroke-width="1" fill="blue" transform="translate(500,500)"></circle><text x="146.66" y="-74.16" transform="translate(515,480)" fill="white" font-size="20">Sinnen</text>
<line stroke-linecap="undefined" stroke-linejoin="undefined" id="svg_1" y2="]]..destY..[[" x2="]]..destX..[[" y1="]]..locY..[[" x1="]]..locX..[[" transform="translate(500,500)" stroke-width="5" stroke="#ff0000" fill="none"/>
<circle cx="]]..locX..[[" cy="]]..locY..[[" r="3" stroke="black" stroke-width="1" fill="limegreen" transform="translate(500,500)"></circle>
<text x="]]..locX..[[" y="]]..locY..[[" transform="translate(500,500)"
fill="limegreen" font-size= "4.5vh" font-weight= "bold">//SHIP POSITION</text>
</svg>
<svg class="bootstrap" viewBox="0 0 1024 612" style="width:100%; height:100%">
<g>
<title>Layer 1</title>
<g id="svg_24">
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_8" y="70" x="55" stroke-width="0" fill="Yellow">Alioth :]]..distalioth..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_14" y="170" x="55" stroke-width="0" fill="Yellow">Madis :]]..distmadis..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_17" y="270" x="55" stroke-width="0" fill="Yellow">Thades :]]..distthades..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_20" y="370" x="55" stroke-width="0" fill="Yellow">Talemai :]]..disttalemai..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_23" y="470" x="55" stroke-width="0" fill="Yellow">Feli :]]..distfeli..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_26" y="570" x="55" stroke-width="0" fill="Yellow">Sicari :]]..distsicari..[[ SU</text>
<g id="svg_12">
<rect rx="10" id="svg_1" height="50" width="250" y="30" x="15" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_3" height="50" width="250" y="105" x="15" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_7" height="50" width="250" y="180" x="15" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_9" height="50" width="250" y="255" x="15" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_10" height="50" width="250" y="330" x="15" stroke-width="20" stroke="#00ff00" fill="none"/>
<rect rx="10" id="svg_11" height="50" width="250" y="405" x="15" stroke-width="20" stroke="#00ff00" fill="none"/>
</g>
</g>
<g id="svg_40">
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_25" y="70" x="997.163642" stroke-width="0" fill="Yellow">Symeon :]]..distsymeon..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_27" y="170" x="997.163642" stroke-width="0" fill="Yellow">Sinnen :]]..distsinnen..[[ SU</text>
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<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_31" y="470" x="997.163642" stroke-width="0" fill="Yellow">Ion :]]..distion..[[ SU</text>
<text stroke="null" transform="matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) " xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="20" id="svg_32" y="570" x="997.163642" stroke-width="0" fill="Yellow">Lacobus :]]..distlacobus..[[ SU</text>
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unit.setTimer("spacemap",.08)
Json Paste
{"slots":{"0":{"name":"screen","type":{"events":[],"methods":[]}},"1":{"name":"core","type":{"events":[],"methods":[]}},"2":{"name":"slot3","type":{"events":[],"methods":[]}},"3":{"name":"slot4","type":{"events":[],"methods":[]}},"4":{"name":"slot5","type":{"events":[],"methods":[]}},"5":{"name":"slot6","type":{"events":[],"methods":[]}},"6":{"name":"slot7","type":{"events":[],"methods":[]}},"7":{"name":"slot8","type":{"events":[],"methods":[]}},"8":{"name":"slot9","type":{"events":[],"methods":[]}},"9":{"name":"slot10","type":{"events":[],"methods":[]}},"-1":{"name":"unit","type":{"events":[],"methods":[]}},"-2":{"name":"system","type":{"events":[],"methods":[]}},"-3":{"name":"library","type":{"events":[],"methods":[]}}},"handlers":[{"code":"MapScreenMouseX = x\nMapScreenMouseY = y\nMapScreenMouseDown = false\nlocal buttonNo = evaluateButtons()\nif MapScreenButtonSelected > 0 and MapScreenButtonSelected == buttonNo then\n onButtonUp(buttonNo)\n onClick(buttonNo)\nend\nMapScreenButtonSelected = -buttonNo","filter":{"args":[{"variable":"*"},{"variable":"*"}],"signature":"mouseUp(x,y)","slotKey":"0"},"key":"0"},{"code":"MapScreenMouseX = x\nMapScreenMouseY = y\nMapScreenMouseDown = true\nMapScreenButtonSelected = evaluateButtons()\nonButtonDown(MapScreenButtonSelected)\n","filter":{"args":[{"variable":"*"},{"variable":"*"}],"signature":"mouseDown(x,y)","slotKey":"0"},"key":"1"},{"code":"function Atlas()\n return {\n [0] = {\n [1]={\n GM=6930729684,\n bodyId=1,\n center={x=17465536.000,y=22665536.000,z=-34464.000},\n name='Madis',\n planetarySystemId=0,\n radius=44300\n },\n [2]={\n GM=157470826617,\n bodyId=2,\n center={x=-8.000,y=-8.000,z=-126303.000},\n name='Alioth',\n planetarySystemId=0,\n radius=126068\n },\n [3]={\n GM=11776905000,\n bodyId=3,\n center={x=29165536.000,y=10865536.000,z=65536.000},\n name='Thades',\n planetarySystemId=0,\n radius=49000\n },\n [4]={\n GM=14893847582,\n bodyId=4,\n center={x=-13234464.000,y=55765536.000,z=465536.000},\n name='Talemai',\n planetarySystemId=0,\n radius=57450\n },\n [5]={\n GM=16951680000,\n bodyId=5,\n center={x=-43534464.000,y=22565536.000,z=-48934464.000},\n name='Feli',\n planetarySystemId=0,\n radius=60000\n },\n [6]={\n GM=10502547741,\n bodyId=6,\n center={x=52765536.000,y=27165538.000,z=52065535.000},\n name='Sicari',\n planetarySystemId=0,\n radius=51100\n },\n [7]={\n GM=13033380591,\n bodyId=7,\n center={x=58665538.000,y=29665535.000,z=58165535.000},\n name='Sinnen',\n planetarySystemId=0,\n radius=54950\n },\n [8]={\n GM=18477723600,\n bodyId=8,\n center={x=80865538.000,y=54665536.000,z=-934463.940},\n name='Teoma',\n planetarySystemId=0,\n radius=62000\n },\n [9]={\n GM=18606274330,\n bodyId=9,\n center={x=-94134462.000,y=12765534.000,z=-3634464.000},\n name='Jago',\n planetarySystemId=0,\n radius=61590\n },\n [10]={\n GM=78480000,\n bodyId=10,\n center={x=17448118.224,y=22966846.286,z=143078.820},\n name='Madis Moon 1',\n planetarySystemId=0,\n radius=10000\n },\n [11]={\n GM=237402000,\n bodyId=11,\n center={x=17194626.000,y=22243633.880,z=-214962.810},\n name='Madis Moon 2',\n planetarySystemId=0,\n radius=11000\n },\n [12]={\n GM=265046609,\n bodyId=12,\n center={x=17520614.000,y=22184730.000,z=-309989.990},\n name='Madis Moon 3',\n planetarySystemId=0,\n radius=15005\n },\n [21]={\n GM=2118960000,\n bodyId=21,\n center={x=457933.000,y=-1509011.000,z=115524.000},\n name='Alioth Moon 1',\n planetarySystemId=0,\n radius=30000\n },\n [22]={\n GM=2165833514,\n bodyId=22,\n center={x=-1692694.000,y=729681.000,z=-411464.000},\n name='Alioth Moon 4',\n planetarySystemId=0,\n radius=30330\n },\n [26]={\n GM=68234043600,\n bodyId=26,\n center={x=-1404835.000,y=562655.000,z=-285074.000},\n name='Sanctuary',\n planetarySystemId=0,\n radius=83400\n },\n [30]={\n GM=211564034,\n bodyId=30,\n center={x=29214402.000,y=10907080.695,z=433858.200},\n name='Thades Moon 1',\n planetarySystemId=0,\n radius=14002\n },\n [31]={\n GM=264870000,\n bodyId=31,\n center={x=29404193.000,y=10432768.000,z=19554.131},\n name='Thades Moon 2',\n planetarySystemId=0,\n radius=15000\n },\n [40]={\n GM=141264000,\n bodyId=40,\n center={x=-13503090.000,y=55594325.000,z=769838.640},\n name='Talemai Moon 2',\n planetarySystemId=0,\n radius=12000\n },\n [41]={\n GM=106830900,\n bodyId=41,\n center={x=-12800515.000,y=55700259.000,z=325207.840},\n name='Talemai Moon 3',\n planetarySystemId=0,\n radius=11000\n },\n [42]={\n GM=264870000,\n bodyId=42,\n center={x=-13058408.000,y=55781856.000,z=740177.760},\n name='Talemai Moon 1',\n planetarySystemId=0,\n radius=15000\n },\n [50]={\n GM=499917600,\n bodyId=50,\n center={x=-43902841.780,y=22261034.700,z=-48862386.000},\n name='Feli Moon 1',\n planetarySystemId=0,\n radius=14000\n },\n [70]={\n GM=396912600,\n bodyId=70,\n center={x=58969616.000,y=29797945.000,z=57969449.000},\n name='Sinnen Moon 1',\n planetarySystemId=0,\n radius=17000\n },\n [100]={\n GM=13975172474,\n bodyId=100,\n center={x=98865536.000,y=-13534464.000,z=-934461.990},\n name='Lacobus',\n planetarySystemId=0,\n radius=55650\n },\n [101]={\n GM=264870000,\n bodyId=101,\n center={x=98905288.170,y=-13950921.100,z=-647589.530},\n name='Lacobus Moon 3',\n planetarySystemId=0,\n radius=15000\n },\n [102]={\n GM=444981600,\n bodyId=102,\n center={x=99180968.000,y=-13783862.000,z=-926156.400},\n name='Lacobus Moon 1',\n planetarySystemId=0,\n radius=18000\n },\n [103]={\n GM=211503600,\n bodyId=103,\n center={x=99250052.000,y=-13629215.000,z=-1059341.400},\n name='Lacobus Moon 2',\n planetarySystemId=0,\n radius=14000\n },\n [110]={\n GM=9204742375,\n bodyId=110,\n center={x=14165536.000,y=-85634465.000,z=-934464.300},\n name='Symeon',\n planetarySystemId=0,\n radius=49050\n },\n [120]={\n GM=7135606629,\n bodyId=120,\n center={x=2865536.700,y=-99034464.000,z=-934462.020},\n name='Ion',\n planetarySystemId=0,\n radius=44950\n },\n [121]={\n GM=106830900,\n bodyId=121,\n center={x=2472916.800,y=-99133747.000,z=-1133582.800},\n name='Ion Moon 1',\n planetarySystemId=0,\n radius=11000\n },\n [122]={\n GM=176580000,\n bodyId=122,\n center={x=2995424.500,y=-99275010.000,z=-1378480.700},\n name='Ion Moon 2',\n planetarySystemId=0,\n radius=15000\n } \n }\n }\n end\nfunction PlanetRef() \n--[[ \n Provide coordinate transforms and access to kinematic related parameters\n Author: JayleBreak\n Usage (unit.start):\n PlanetaryReference = require('planetref')\n galaxyReference = PlanetaryReference(referenceTableSource)\n helios = galaxyReference[0] -- PlanetaryReference.PlanetarySystem instance\n alioth = helios[2] -- PlanetaryReference.BodyParameters instance\n Methods:\n PlanetaryReference:getPlanetarySystem - based on planetary system ID.\n PlanetaryReference.isMapPosition - 'true' if an instance of 'MapPosition'\n PlanetaryReference.createBodyParameters - for entry into reference table\n PlanetaryReference.BodyParameters - a class containing a body's information.\n PlanetaryReference.MapPosition - a class for map coordinates\n PlanetaryReference.PlanetarySystem - a container for planetary system info.\n PlanetarySystem:castIntersections - from a position in a given direction.\n PlanetarySystem:closestBody - to the specified coordinates.\n PlanetarySystem:convertToBodyIdAndWorldCoordinates - from map coordinates.\n PlanetarySystem:getBodyParameters - from reference table.\n PlanetarySystem:getPlanetarySystemId - for the instance.\n BodyParameters:convertToWorldCoordinates - from map coordinates\n BodyParameters:convertToMapPosition - from world coordinates\n BodyParameters:getAltitude - of world coordinates\n BodyParameters:getDistance - from center to world coordinates\n BodyParameters:getGravity - at a given position in world coordinates.\n Description\n An instance of the 'PlanetaryReference' \"class\" can contain transform and\n kinematic reference information for all planetary systems in DualUniverse.\n Each planetary system is identified by a numeric identifier. Currently,\n the only planetary system, Helios, has the identifier: zero. This \"class\"\n supports the indexing ('[]') operation which is equivalent to the\n use of the 'getPlanetarySystem' method. It also supports the 'pairs()'\n method for iterating over planetary systems.\n\n An instance of the 'PlanetarySystem' \"class\" contains all reference\n information for a specific system. It supports the indexing ('[]') and\n 'pairs()' functions which allows iteration over each \"body\" in the\n system where the key is the numeric body ID. It also supports the\n 'tostring()' method.\n An instance of the 'BodyParameters' \"class\" contains all reference\n information for a single celestial \"body\" (a moon or planet). It supports\n the 'tostring()' method, and contains the data members:\n planetarySystemId - numeric planetary system ID\n bodyId - numeric body ID\n radius - radius of the body in meters (zero altitude)\n center - world coordinates of the body's center position\n GM - the gravitation parameter (g = GM/radius^2)\n Note that the user is allowed to add custom fields (e.g. body name), but\n should insure that complex table values have the '__tostring' metamethod\n implemented.\n Transform and Kinematics:\n \"World\" coordinates is a cartesian coordinate system with an origin at an\n arbitrary fixed point in a planetary system and with distances measured in\n meters. The coordinates are expressible either as a simple table of 3 values\n or an instance of the 'vec3' class. In either case, the planetary system\n identity is implicit.\n \"Map\" coordinates is a geographic coordinate system with an origin at the\n center of an identified (by a numeric value) celestial body which is a\n member of an identified (also a numeric value) planetary system. Note that\n the convention that latitude, longitude, and altitude values will be the\n position's x, y, and z world coordinates in the special case of body ID 0.\n The kinematic parameters in the reference data permit calculations of the\n gravitational attraction of the celestial body on other objects.\n Reference Data:\n This is an example of reference data with a single entry assigned to\n planetary system ID 0, and body ID 2 ('Alioth'):\n referenceTable = {\n [0] = { [2] = { planetarySystemId = 0,\n bodyId = 2,\n radius = 126068,\n center = vec3({x=-8, y=-8, z=-126303}),\n GM = 1.572199+11 } -- as in F=-GMm/r^2\n }\n }\n ref=PlanetaryReference(referenceTable)\n Collecting Reference Data:\n A combination of information from the \"Map\" screen in the DU user interface,\n and values reported by the DU Lua API can be the source of the reference\n table's data (planetarySystemId, bodyId, and surfaceArea is from the user\n interface):\n referenceTable = {}\n referenceTable[planetarySystemId][bodyId] =\n PlanetaryReference.createBodyParameters(planetarySystemId,\n bodyId,\n surfaceArea,\n core.getConstructWorldPos(),\n core.getWorldVertical(),\n core.getAltitude(),\n core.g())\n Adapting Data Sources:\n Other sources of data can be adapted or converted. An example of adapting a\n table, defined in the file: 'planets.lua', containing information on a single\n planetary system and using celestial body name as the key follows (note that\n a 'name' field is added to the BodyParameters instance transparently after\n construction, and the '__pairs' meta function is required to support the\n 'closestBody' and '__tostring' methods):\n ref=PlanetaryReference(\n {[0] = setmetatable(require('planets'),\n { __index = function(bodies, bodyId)\n for _,v in pairs(bodies) do\n if v and v.bodyId == bodyId then return v end\n end\n return nil\n end,\n __pairs = function(bodies)\n return function(t, k)\n local nk, nv = next(t, k)\n if nv then\n local GM = nv.gravity * nv.radius^2\n local bp = BodyParameters(0,\n nv.id,\n nv.radius,\n nv.pos,\n GM)\n bp.name = nk\n return nk, bp\n end\n return nk, nv\n end, bodies, nil\n end })\n })\n\n Converting Data Sources:\n An instance of 'PlanetaryReference' that has been adapted to a data source\n can be used to convert that source to simple table. For example,\n using the adapted instance shown above:\n load('convertedData=' .. tostring(ref))()\n newRef=PlanetaryReference(convertedData)\n Also See: kepler.lua\n ]]--\n--[[ START OF LOCAL IMPLEMENTATION DETAILS ]]--\n-- Type checks\nlocal function isNumber(n) return type(n) == 'number' end\nlocal function isSNumber(n) return type(tonumber(n)) == 'number' end\nlocal function isTable(t) return type(t) == 'table' end\nlocal function isString(s) return type(s) == 'string' end\nlocal function isVector(v) return isTable(v)\n and isNumber(v.x and v.y and v.z) end\nlocal function isMapPosition(m) return isTable(m) and isNumber(m.latitude and\n m.longitude and\n m.altitude and\n m.bodyId and\n m.systemId) end\n-- Constants\nlocal deg2rad = math.pi/180\nlocal rad2deg = 180/math.pi\nlocal epsilon = 1e-10\nlocal num = ' *([+-]?%d+%.?%d*e?[+-]?%d*)'\nlocal posPattern = '::pos{' .. num .. ',' .. num .. ',' .. num .. ',' ..\n num .. ',' .. num .. '}'\n-- Utilities\nlocal utils = require('cpml.utils')\nlocal vec3 = require('cpml.vec3')\nlocal clamp = utils.clamp\nlocal function float_eq(a,b)\n if a == 0 then return math.abs(b) < 1e-09 end\n if b == 0 then return math.abs(a) < 1e-09 end\n return math.abs(a - b) < math.max(math.abs(a),math.abs(b))*epsilon\nend\nlocal function formatNumber(n)\n local result = string.gsub(\n string.reverse(string.format('%.4f',n)),\n '^0*%.?','')\n return result == '' and '0' or string.reverse(result)\nend\nlocal function formatValue(obj)\n if isVector(obj) then\n return string.format('{x=%.3f,y=%.3f,z=%.3f}', obj.x, obj.y, obj.z)\n end\n if isTable(obj) and not getmetatable(obj) then\n local list = {}\n local nxt = next(obj)\n if type(nxt) == 'nil' or nxt == 1 then -- assume this is an array\n list = obj\n else\n for k,v in pairs(obj) do\n local value = formatValue(v)\n if type(k) == 'number' then\n table.insert(list, string.format('[%s]=%s', k, value))\n else\n table.insert(list, string.format('%s=%s', k, value))\n end\n end\n end\n return string.format('{%s}', table.concat(list, ','))\n end\n if isString(obj) then\n return string.format(\"'%s'\", obj:gsub(\"'\",[[\\']]))\n end\n return tostring(obj)\nend\n-- CLASSES\n-- BodyParameters: Attributes of planetary bodies (planets and moons)\nlocal BodyParameters = {}\nBodyParameters.__index = BodyParameters\nBodyParameters.__tostring =\n function(obj, indent)\n local sep = indent or ''\n local keys = {}\n for k in pairs(obj) do table.insert(keys, k) end\n table.sort(keys)\n local list = {}\n for _, k in ipairs(keys) do\n local value = formatValue(obj[k])\n if type(k) == 'number' then\n table.insert(list, string.format('[%s]=%s', k, value))\n else\n table.insert(list, string.format('%s=%s', k, value))\n end\n end\n if indent then\n return string.format('%s%s',\n indent,\n table.concat(list, ',\\n' .. indent))\n end\n return string.format('{%s}', table.concat(list, ','))\n end\nBodyParameters.__eq = function(lhs, rhs)\n return lhs.planetarySystemId == rhs.planetarySystemId and\n lhs.bodyId == rhs.bodyId and\n float_eq(lhs.radius, rhs.radius) and\n float_eq(lhs.center.x, rhs.center.x) and\n float_eq(lhs.center.y, rhs.center.y) and\n float_eq(lhs.center.z, rhs.center.z) and\n float_eq(lhs.GM, rhs.GM)\n end\nlocal function mkBodyParameters(systemId, bodyId, radius, worldCoordinates, GM)\n -- 'worldCoordinates' can be either table or vec3\n assert(isSNumber(systemId),\n 'Argument 1 (planetarySystemId) must be a number:' .. type(systemId))\n assert(isSNumber(bodyId),\n 'Argument 2 (bodyId) must be a number:' .. type(bodyId))\n assert(isSNumber(radius),\n 'Argument 3 (radius) must be a number:' .. type(radius))\n assert(isTable(worldCoordinates),\n 'Argument 4 (worldCoordinates) must be a array or vec3.' ..\n type(worldCoordinates))\n assert(isSNumber(GM),\n 'Argument 5 (GM) must be a number:' .. type(GM))\n return setmetatable({planetarySystemId = tonumber(systemId),\n bodyId = tonumber(bodyId),\n radius = tonumber(radius),\n center = vec3(worldCoordinates),\n GM = tonumber(GM) }, BodyParameters)\nend\n-- MapPosition: Geographical coordinates of a point on a planetary body.\nlocal MapPosition = {}\nMapPosition.__index = MapPosition\nMapPosition.__tostring = function(p)\n return string.format('::pos{%d,%d,%s,%s,%s}',\n p.systemId,\n p.bodyId,\n formatNumber(p.latitude*rad2deg),\n formatNumber(p.longitude*rad2deg),\n formatNumber(p.altitude))\n end\nMapPosition.__eq = function(lhs, rhs)\n return lhs.bodyId == rhs.bodyId and\n lhs.systemId == rhs.systemId and\n float_eq(lhs.latitude, rhs.latitude) and\n float_eq(lhs.altitude, rhs.altitude) and\n (float_eq(lhs.longitude, rhs.longitude) or\n float_eq(lhs.latitude, math.pi/2) or\n float_eq(lhs.latitude, -math.pi/2))\n end\n-- latitude and longitude are in degrees while altitude is in meters\nlocal function mkMapPosition(overload, bodyId, latitude, longitude, altitude)\n local systemId = overload -- Id or '::pos{...}' string\n if isString(overload) and not longitude and not altitude and\n not bodyId and not latitude then\n systemId, bodyId, latitude, longitude, altitude =\n string.match(overload, posPattern)\n assert(systemId, 'Argument 1 (position string) is malformed.')\n else\n assert(isSNumber(systemId),\n 'Argument 1 (systemId) must be a number:' .. type(systemId))\n assert(isSNumber(bodyId),\n 'Argument 2 (bodyId) must be a number:' .. type(bodyId))\n assert(isSNumber(latitude),\n 'Argument 3 (latitude) must be in degrees:' .. type(latitude))\n assert(isSNumber(longitude),\n 'Argument 4 (longitude) must be in degrees:' .. type(longitude))\n assert(isSNumber(altitude),\n 'Argument 5 (altitude) must be in meters:' .. type(altitude))\n end\n systemId = tonumber(systemId)\n bodyId = tonumber(bodyId)\n latitude = tonumber(latitude)\n longitude = tonumber(longitude)\n altitude = tonumber(altitude)\n if bodyId == 0 then -- this is a hack to represent points in space\n return setmetatable({latitude = latitude,\n longitude = longitude,\n altitude = altitude,\n bodyId = bodyId,\n systemId = systemId}, MapPosition)\n end\n return setmetatable({latitude = deg2rad*clamp(latitude, -90, 90),\n longitude = deg2rad*(longitude % 360),\n altitude = altitude,\n bodyId = bodyId,\n systemId = systemId}, MapPosition)\nend\n-- PlanetarySystem - map body IDs to BodyParameters\nlocal PlanetarySystem = {}\nPlanetarySystem.__index = PlanetarySystem\nPlanetarySystem.__tostring =\n function (obj, indent)\n local sep = indent and (indent .. ' ' )\n local bdylist = {}\n local keys = {}\n for k in pairs(obj) do table.insert(keys, k) end\n table.sort(keys)\n for _, bi in ipairs(keys) do\n bdy = obj[bi]\n local bdys = BodyParameters.__tostring(bdy, sep)\n if indent then\n table.insert(bdylist,\n string.format('[%s]={\\n%s\\n%s}',\n bi, bdys, indent))\n else\n table.insert(bdylist, string.format(' [%s]=%s', bi, bdys))\n end\n end\n if indent then\n return string.format('\\n%s%s%s',\n indent,\n table.concat(bdylist, ',\\n' .. indent),\n indent)\n end\n return string.format('{\\n%s\\n}', table.concat(bdylist, ',\\n'))\n end\nlocal function mkPlanetarySystem(referenceTable)\n local atlas = {}\n local pid\n for _, v in pairs(referenceTable) do\n local id = v.planetarySystemId\n if type(id) ~= 'number' then\n error('Invalid planetary system ID: ' .. tostring(id))\n elseif pid and id ~= pid then\n error('Mismatch planetary system IDs: ' .. id .. ' and '\n .. pid)\n end\n local bid = v.bodyId\n if type(bid) ~= 'number' then\n error('Invalid body ID: ' .. tostring(bid))\n elseif atlas[bid] then\n error('Duplicate body ID: ' .. tostring(bid))\n end\n setmetatable(v.center, getmetatable(vec3.unit_x))\n atlas[bid] = setmetatable(v, BodyParameters)\n pid = id\n end\n return setmetatable(atlas, PlanetarySystem)\nend\n-- PlanetaryReference - map planetary system ID to PlanetarySystem\nPlanetaryReference = {}\nlocal function mkPlanetaryReference(referenceTable)\n return setmetatable({ galaxyAtlas = referenceTable or {} },\n PlanetaryReference)\nend\nPlanetaryReference.__index = \n function(t,i)\n if type(i) == 'number' then\n local system = t.galaxyAtlas[i]\n return mkPlanetarySystem(system)\n end\n return rawget(PlanetaryReference, i)\n end\nPlanetaryReference.__pairs =\n function(obj)\n return function(t, k)\n local nk, nv = next(t, k)\n return nk, nv and mkPlanetarySystem(nv)\n end, obj.galaxyAtlas, nil\n end\nPlanetaryReference.__tostring =\n function (obj)\n local pslist = {}\n for _,ps in pairs(obj or {}) do\n local psi = ps:getPlanetarySystemId()\n local pss = PlanetarySystem.__tostring(ps, ' ')\n table.insert(pslist,\n string.format(' [%s]={%s\\n }', psi, pss))\n end\n return string.format('{\\n%s\\n}\\n', table.concat(pslist,',\\n'))\n end\n--[[ START OF PUBLIC INTERFACE ]]--\n-- PlanetaryReference CLASS METHODS:\n--\n-- BodyParameters - create an instance of BodyParameters class\n-- planetarySystemId [in]: the body's planetary system ID.\n-- bodyId [in]: the body's ID.\n-- radius [in]: the radius in meters of the planetary body.\n-- bodyCenter [in]: the world coordinates of the center (vec3 or table).\n-- GM [in]: the body's standard gravitational parameter.\n-- return: an instance of BodyParameters class.\n--\nPlanetaryReference.BodyParameters = mkBodyParameters\n--\n-- MapPosition - create an instance of the MapPosition class\n-- overload [in]: either a planetary system ID or a position string ('::pos...')\n-- bodyId [in]: (ignored if overload is a position string) the body's ID.\n-- latitude [in]: (ignored if overload is a position string) the latitude.\n-- longitude [in]:(ignored if overload is a position string) the longitude.\n-- altitude [in]: (ignored if overload is a position string) the altitude.\n-- return: the class instance\n--\nPlanetaryReference.MapPosition = mkMapPosition\n--\n-- PlanetarySystem - create an instance of PlanetarySystem class\n-- referenceData [in]: a table (indexed by bodyId) of body reference info.\n-- return: the class instance\n--\nPlanetaryReference.PlanetarySystem = mkPlanetarySystem\n--\n-- createBodyParameters - create an instance of BodyParameters class\n-- planetarySystemId [in]: the body's planetary system ID.\n-- bodyId [in]: the body's ID.\n-- surfaceArea [in]: the body's surface area in square meters.\n-- aPosition [in]: world coordinates of a position near the body.\n-- verticalAtPosition [in]: a vector pointing towards the body center.\n-- altitudeAtPosition [in]: the altitude in meters at the position.\n-- gravityAtPosition [in]: the magnitude of the gravitational acceleration.\n-- return: an instance of BodyParameters class.\n--\nfunction PlanetaryReference.createBodyParameters(planetarySystemId,\n bodyId,\n surfaceArea,\n aPosition,\n verticalAtPosition,\n altitudeAtPosition,\n gravityAtPosition)\n assert(isSNumber(planetarySystemId),\n 'Argument 1 (planetarySystemId) must be a number:' ..\n type(planetarySystemId))\n assert(isSNumber(bodyId),\n 'Argument 2 (bodyId) must be a number:' .. type(bodyId))\n assert(isSNumber(surfaceArea),\n 'Argument 3 (surfaceArea) must be a number:' .. type(surfaceArea))\n assert(isTable(aPosition),\n 'Argument 4 (aPosition) must be an array or vec3:' ..\n type(aPosition))\n assert(isTable(verticalAtPosition),\n 'Argument 5 (verticalAtPosition) must be an array or vec3:' ..\n type(verticalAtPosition))\n assert(isSNumber(altitudeAtPosition),\n 'Argument 6 (altitude) must be in meters:' ..\n type(altitudeAtPosition))\n assert(isSNumber(gravityAtPosition),\n 'Argument 7 (gravityAtPosition) must be number:' ..\n type(gravityAtPosition))\n local radius = math.sqrt(surfaceArea/4/math.pi)\n local distance = radius + altitudeAtPosition\n local center = vec3(aPosition) + distance*vec3(verticalAtPosition)\n local GM = gravityAtPosition * distance * distance\n return mkBodyParameters(planetarySystemId, bodyId, radius, center, GM)\nend\n--\n-- isMapPosition - check for the presence of the 'MapPosition' fields\n-- valueToTest [in]: the value to be checked\n-- return: 'true' if all required fields are present in the input value\n--\nPlanetaryReference.isMapPosition = isMapPosition\n-- PlanetaryReference INSTANCE METHODS:\n--\n-- getPlanetarySystem - get the planetary system using ID or MapPosition as key\n-- overload [in]: either the planetary system ID or a MapPosition that has it.\n-- return: instance of 'PlanetarySystem' class or nil on error\n--\nfunction PlanetaryReference:getPlanetarySystem(overload)\n --if galaxyAtlas then\n local planetarySystemId = overload\n if isMapPosition(overload) then\n planetarySystemId = overload.systemId\n end\n if type(planetarySystemId) == 'number' then\n local system = self.galaxyAtlas[i]\n if system then\n if getmetatable(nv) ~= PlanetarySystem then\n system = mkPlanetarySystem(system)\n end\n return system\n end\n end\n --end\n --return nil\nend\n-- PlanetarySystem INSTANCE METHODS:\n--\n-- castIntersections - Find the closest body that intersects a \"ray cast\".\n-- origin [in]: the origin of the \"ray cast\" in world coordinates\n-- direction [in]: the direction of the \"ray cast\" as a 'vec3' instance.\n-- sizeCalculator [in]: (default: returns 1.05*radius) Returns size given body.\n-- bodyIds[in]: (default: all IDs in system) check only the given IDs.\n-- return: The closest body that blocks the cast or 'nil' if none.\n--\nfunction PlanetarySystem:castIntersections(origin,\n direction,\n sizeCalculator,\n bodyIds)\n local sizeCalculator = sizeCalculator or \n function (body) return 1.05*body.radius end\n local candidates = {}\n if bodyIds then\n for _,i in ipairs(bodyIds) do candidates[i] = self[i] end\n else\n bodyIds = {}\n for k,body in pairs(self) do\n table.insert(bodyIds, k)\n candidates[k] = body\n end\n end\n local function compare(b1,b2)\n local v1 = candidates[b1].center - origin\n local v2 = candidates[b2].center - origin\n return v1:len() < v2:len()\n end\n table.sort(bodyIds, compare)\n local dir = direction:normalize()\n for i, id in ipairs(bodyIds) do\n local body = candidates[id]\n local c_oV3 = body.center - origin\n local radius = sizeCalculator(body)\n local dot = c_oV3:dot(dir)\n local desc = dot^2 - (c_oV3:len2() - radius^2)\n if desc >= 0 then\n local root = math.sqrt(desc)\n local farSide = dot + root\n local nearSide = dot - root\n if nearSide > 0 then\n return body, farSide, nearSide\n elseif farSide > 0 then\n return body, farSide, nil\n end\n end\n end\n return nil, nil, nil\nend\n--\n-- closestBody - find the closest body to a given set of world coordinates\n-- coordinates [in]: the world coordinates of position in space\n-- return: an instance of the BodyParameters object closest to 'coordinates'\n--\nfunction PlanetarySystem:closestBody(coordinates)\n assert(type(coordinates) == 'table', 'Invalid coordinates.')\n local minDistance2, body\n local coord = vec3(coordinates)\n for _,params in pairs(self) do\n local distance2 = (params.center - coord):len2()\n if not body or distance2 < minDistance2 then\n body = params\n minDistance2 = distance2\n end\n end\n return body\nend\n--\n-- convertToBodyIdAndWorldCoordinates - map to body Id and world coordinates\n-- overload [in]: an instance of MapPosition or a position string ('::pos...)\n-- return: a vec3 instance containing the world coordinates or 'nil' on error.\n--\nfunction PlanetarySystem:convertToBodyIdAndWorldCoordinates(overload)\n local mapPosition = overload\n if isString(overload) then\n mapPosition = mkMapPosition(overload)\n end\n if mapPosition.bodyId == 0 then\n return 0, vec3(mapPosition.latitude,\n mapPosition.longitude,\n mapPosition.altitude)\n end\n local params = self:getBodyParameters(mapPosition)\n if params then\n return mapPosition.bodyId,\n params:convertToWorldCoordinates(mapPosition)\n end\nend\n--\n-- getBodyParameters - get or create an instance of BodyParameters class\n-- overload [in]: either an instance of MapPosition or a body's ID.\n-- return: a BodyParameters instance or 'nil' if body ID is not found.\n--\nfunction PlanetarySystem:getBodyParameters(overload)\n local bodyId = overload\n if isMapPosition(overload) then\n bodyId = overload.bodyId\n end\n assert(isSNumber(bodyId),\n 'Argument 1 (bodyId) must be a number:' .. type(bodyId))\n return self[bodyId]\nend\n--\n-- getPlanetarySystemId - get the planetary system ID for this instance\n-- return: the planetary system ID or nil if no planets are in the system.\n--\nfunction PlanetarySystem:getPlanetarySystemId()\n local k, v = next(self)\n return v and v.planetarySystemId\nend\n-- BodyParameters INSTANCE METHODS:\n--\n-- convertToMapPosition - create an instance of MapPosition from coordinates\n-- worldCoordinates [in]: the world coordinates of the map position.\n-- return: an instance of MapPosition class\n--\nfunction BodyParameters:convertToMapPosition(worldCoordinates)\n assert(isTable(worldCoordinates),\n 'Argument 1 (worldCoordinates) must be an array or vec3:' ..\n type(worldCoordinates))\n local worldVec = vec3(worldCoordinates) \n if self.bodyId == 0 then\n return setmetatable({latitude = worldVec.x,\n longitude = worldVec.y,\n altitude = worldVec.z,\n bodyId = 0,\n systemId = self.planetarySystemId}, MapPosition)\n end\n local coords = worldVec - self.center\n local distance = coords:len()\n local altitude = distance - self.radius\n local latitude = 0\n local longitude = 0\n if not float_eq(distance, 0) then\n local phi = math.atan(coords.y, coords.x)\n longitude = phi >= 0 and phi or (2*math.pi + phi)\n latitude = math.pi/2 - math.acos(coords.z/distance)\n end\n return setmetatable({latitude = latitude,\n longitude = longitude,\n altitude = altitude,\n bodyId = self.bodyId,\n systemId = self.planetarySystemId}, MapPosition)\nend\n--\n-- convertToWorldCoordinates - convert a map position to world coordinates\n-- overload [in]: an instance of MapPosition or a position string ('::pos...')\n--\nfunction BodyParameters:convertToWorldCoordinates(overload)\n local mapPosition = isString(overload) and\n mkMapPosition(overload) or overload\n if mapPosition.bodyId == 0 then -- support deep space map position\n return vec3(mapPosition.latitude,\n mapPosition.longitude,\n mapPosition.altitude)\n end\n assert(isMapPosition(mapPosition),\n 'Argument 1 (mapPosition) is not an instance of \"MapPosition\".')\n assert(mapPosition.systemId == self.planetarySystemId,\n 'Argument 1 (mapPosition) has a different planetary system ID.')\n assert(mapPosition.bodyId == self.bodyId,\n 'Argument 1 (mapPosition) has a different planetary body ID.')\n local xproj = math.cos(mapPosition.latitude)\n return self.center + (self.radius + mapPosition.altitude) *\n vec3(xproj*math.cos(mapPosition.longitude),\n xproj*math.sin(mapPosition.longitude),\n math.sin(mapPosition.latitude))\nend\n--\n-- getAltitude - calculate the altitude of a point given in world coordinates.\n-- worldCoordinates [in]: the world coordinates of the point.\n-- return: the altitude in meters\n--\nfunction BodyParameters:getAltitude(worldCoordinates)\n return (vec3(worldCoordinates) - self.center):len() - self.radius\nend\n--\n-- getDistance - calculate the distance to a point given in world coordinates.\n-- worldCoordinates [in]: the world coordinates of the point.\n-- return: the distance in meters\n--\nfunction BodyParameters:getDistance(worldCoordinates)\n return (vec3(worldCoordinates) - self.center):len()\nend\n--\n-- getGravity - calculate the gravity vector induced by the body.\n-- worldCoordinates [in]: the world coordinates of the point.\n-- return: the gravity vector in meter/seconds^2\n--\nfunction BodyParameters:getGravity(worldCoordinates)\n local radial = self.center - vec3(worldCoordinates) -- directed towards body\n local len2 = radial:len2()\n return (self.GM/len2) * radial/math.sqrt(len2)\nend\n-- end of module\nreturn setmetatable(PlanetaryReference,\n { __call = function(_,...)\n return mkPlanetaryReference(...)\n end })\nend\nfunction Keplers()\n --[[ \n Provides methods for computing orbital information for an object\n Usage:\n Kepler = require('autoconf.custom.kepler')\n alioth = Kepler({ GM=157470826617,\n bodyId=2,\n center={x=-8.000,y=-8.000,z=-126303.000},\n name='Alioth',\n planetarySystemId=0,\n radius=126068\n })\n altitude = 6000\n position = '::pos{0,2,0,0,6000}'\n e, o = alioth:escapeAndOrbitalSpeed(altitude)\n orbit = alioth:orbitalParameters(position, {0, o+1, 0})\n print(\"Eccentricity \" .. orbit.eccentricity)\n print(\"Perihelion \" .. orbit.periapsis.altitude)\n print(\"Max. speed \" .. orbit.periapsis.speed)\n print(\"Circular orbit speed \" .. orbit.periapsis.circularOrbitSpeed)\n print(\"Aphelion \" .. orbit.apoapsis.altitude)\n print(\"Min. speed \" .. orbit.apoapsis.speed)\n print(\"Orbital period \" .. orbit.period)\n --- output:\n Eccentricity 0.0018324307017878\n Perihelion 6000.0\n Max. speed 1092.9462297033\n Circular orbit speed 1091.9462297033\n Aphelion 6484.8994605062\n Min. speed 1088.9480596194\n Orbital period 762.02818214049\n Methods:\n Kepler:escapeAndOrbitalSpeed - for a given celestial body and altitude.\n Kepler:orbitalParameters - for a given massless object and a celestial body.\n Description\n The motion of an object in the vicinity of substantially larger mass is\n in the domain of the \"2-body problem\". By assuming the object whose motion\n is of interest is of negligable mass simplifies the calculations of:\n the speed to escape the body, the speed of a circular orbit, and the\n parameters defining the orbit of the object (or the lack of orbit as the\n case may be).\n Orbital Parameters:\n periapsis - the closest approach to the planet\n apoapsis - the furthest point from the planet if in orbit (otherwise nil)\n eccentricity - 0 for circular orbits\n <1 for elliptical orbits\n 1 for parabiolic trajectory\n >1 for hyperbolic trajectory\n period - time (in seconds) to complete an orbit\n Also See: planetref.lua\n]]--\nlocal vec3 = require('cpml.vec3')\nlocal PlanetRef = PlanetRef()\nlocal function isString(s) return type(s) == 'string' end\nlocal function isTable(t) return type(t) == 'table' end\nlocal function float_eq(a,b)\n if a == 0 then return math.abs(b) < 1e-09 end\n if b == 0 then return math.abs(a) < 1e-09 end\n return math.abs(a - b) < math.max(math.abs(a),math.abs(b))*epsilon\nend\nKepler = {}\nKepler.__index = Kepler\n--\n-- escapeAndOrbitalSpeed - speed required to escape and for a circular orbit\n-- altitude [in]: the height of the orbit in meters above \"sea-level\"\n-- return: the speed in m/s needed to escape the celestial body and to orbit it.\n--\nfunction Kepler:escapeAndOrbitalSpeed(altitude)\n assert(self.body)\n -- P = -GMm/r and KE = mv^2/2 (no lorentz factor used)\n -- mv^2/2 = GMm/r\n -- v^2 = 2GM/r\n -- v = sqrt(2GM/r1)\n local distance = altitude + self.body.radius\n if not float_eq(distance, 0) then\n local orbit = math.sqrt(self.body.GM/distance)\n return math.sqrt(2)*orbit, orbit\n end\n return nil, nil\nend\n--\n-- orbitalParameters: determine the orbital elements for a two-body system.\n-- overload [in]: the world coordinates or map coordinates of a massless object.\n-- velocity [in]: The velocity of the massless point object in m/s.\n-- return: the 6 orbital elements for the massless object.\n--\nfunction Kepler:orbitalParameters(overload, velocity)\n assert(self.body)\n assert(isTable(overload) or isString(overload))\n assert(isTable(velocity))\n local pos = (isString(overload) or PlanetRef.isMapPosition(overload)) and\n self.body:convertToWorldCoordinates(overload) or\n vec3(overload)\n local v = vec3(velocity)\n local r = pos - self.body.center\n local v2 = v:len2()\n local d = r:len()\n local mu = self.body.GM\n local e = ((v2 - mu/d)*r - r:dot(v)*v)/mu\n local a = mu/(2*mu/d - v2)\n local ecc = e:len()\n local dir = e:normalize()\n local pd = a*(1-ecc)\n local ad = a*(1+ecc)\n local per = pd*dir + self.body.center\n local apo = ecc <= 1 and -ad*dir + self.body.center or nil\n local trm = math.sqrt(a*mu*(1-ecc*ecc)) \n local Period = apo and 2*math.pi*math.sqrt(a^3/mu)\n -- These are great and all, but, I need more.\n local trueAnomaly = math.acos((e:dot(r))/(ecc*d))\n if r:dot(v) < 0 then\n trueAnomaly = -(trueAnomaly - 2*math.pi)\n end \n -- Apparently... cos(EccentricAnomaly) = (cos(trueAnomaly) + eccentricity)/(1 + eccentricity * cos(trueAnomaly))\n local EccentricAnomaly = math.acos((math.cos(trueAnomaly) + ecc)/(1 + ecc * math.cos(trueAnomaly)))\n -- Then.... apparently if this is below 0, we should add 2pi to it\n -- I think also if it's below 0, we're past the apoapsis?\n local timeTau = EccentricAnomaly\n if timeTau < 0 then\n timeTau = timeTau + 2*math.pi\n end\n -- So... time since periapsis...\n -- Is apparently easy if you get mean anomly. t = M/n where n is mean motion, = 2*pi/Period\n \n \n local MeanAnomaly = timeTau - ecc * math.sin(timeTau)\n local TimeSincePeriapsis = MeanAnomaly/(2*math.pi/Period)\n --system.print(MeanAnomaly .. \" - \" .. TimeSincePeriapsis .. \" - \" .. Period .. \" - \" .. EccentricAnomaly .. \" - \" .. timeTau .. \" - \" .. trueAnomaly)\n -- Mean anom is 0 at periapsis, positive before it... and positive after it.\n -- I guess this is why I needed to use timeTau and not EccentricAnomaly here\n \n local TimeToPeriapsis = Period - TimeSincePeriapsis\n local TimeToApoapsis = TimeToPeriapsis + Period/2\n if trueAnomaly - math.pi > 0 then -- TBH I think something's wrong in my formulas because I needed this.\n TimeToPeriapsis = TimeSincePeriapsis\n TimeToApoapsis = TimeToPeriapsis + Period/2\n end\n if TimeToApoapsis > Period then\n TimeToApoapsis = TimeToApoapsis - Period\n end\n return { periapsis = { position = per,\n speed = trm/pd,\n circularOrbitSpeed = math.sqrt(mu/pd),\n altitude = pd - self.body.radius},\n apoapsis = apo and\n { position = apo,\n speed = trm/ad,\n circularOrbitSpeed = math.sqrt(mu/ad),\n altitude = ad - self.body.radius},\n currentVelocity = v,\n currentPosition = pos,\n eccentricity = ecc,\n period = Period,\n eccentricAnomaly = EccentricAnomaly,\n meanAnomaly = MeanAnomaly,\n timeToPeriapsis = TimeToPeriapsis,\n timeToApoapsis = TimeToApoapsis\n }\nend\n\nlocal function new(bodyParameters)\n local params = PlanetRef.BodyParameters(bodyParameters.planetarySystemId,\n bodyParameters.bodyId,\n bodyParameters.radius,\n bodyParameters.center,\n bodyParameters.GM)\n return setmetatable({body = params}, Kepler)\nend\nreturn setmetatable(Kepler, { __call = function(_,...) return new(...) end })\nend\nfunction Kinematics()\n --[[ \n DualUniverse kinematic equations\n Author: JayleBreak\n Usage (unit.start):\n Kinematics = require('autoconf.custom.kinematics')\n Methods:\n computeAccelerationTime - \"relativistic\" version of t = (vf - vi)/a\n computeDistanceAndTime - Return distance & time needed to reach final speed.\n computeTravelTime - \"relativistic\" version of t=(sqrt(2ad+v^2)-v)/a\n Description\n DualUniverse increases the effective mass of constructs as their absolute\n speed increases by using the \"lorentz\" factor (from relativity) as the scale\n factor. This results in an upper bound on the absolute speed of constructs\n (excluding \"warp\" drive) that is set to 30 000 KPH (8 333 MPS). This module\n provides utilities for computing some physical quantities taking this\n scaling into account.\n]]--\nlocal Kinematic = {} -- just a namespace\nlocal C = 30000000/3600\nlocal C2 = C*C\nlocal ITERATIONS = 100 -- iterations over engine \"warm-up\" period\nlocal function lorentz(v) return 1/math.sqrt(1 - v*v/C2) end\n--\n-- computeAccelerationTime - \"relativistic\" version of t = (vf - vi)/a\n-- initial [in]: initial (positive) speed in meters per second.\n-- acceleration [in]: constant acceleration until 'finalSpeed' is reached.\n-- final [in]: the speed at the end of the time interval.\n-- return: the time in seconds spent in traversing the distance\n--\nfunction Kinematic.computeAccelerationTime(initial, acceleration, final)\n -- The low speed limit of following is: t=(vf-vi)/a (from: vf=vi+at)\n local k1 = C*math.asin(initial/C)\n return (C * math.asin(final/C) - k1)/acceleration\nend\n--\n-- computeDistanceAndTime - Return distance & time needed to reach final speed.\n-- initial[in]: Initial speed in meters per second.\n-- final[in]: Final speed in meters per second.\n-- restMass[in]: Mass of the construct at rest in Kg.\n-- thrust[in]: Engine's maximum thrust in Newtons.\n-- t50[in]: (default: 0) Time interval to reach 50% thrust in seconds.\n-- brakeThrust[in]: (default: 0) Constant thrust term when braking.\n-- return: Distance (in meters), time (in seconds) required for change.\n--\nfunction Kinematic.computeDistanceAndTime(initial,\n final,\n restMass,\n thrust,\n t50,\n brakeThrust)\n -- This function assumes that the applied thrust is colinear with the\n -- velocity. Furthermore, it does not take into account the influence\n -- of gravity, not just in terms of its impact on velocity, but also\n -- its impact on the orientation of thrust relative to velocity.\n -- These factors will introduce (usually) small errors which grow as\n -- the length of the trip increases.\n t50 = t50 or 0\n brakeThrust = brakeThrust or 0 -- usually zero when accelerating\n local tau0 = lorentz(initial)\n local speedUp = initial <= final\n local a0 = thrust * (speedUp and 1 or -1)/restMass\n local b0 = -brakeThrust/restMass\n local totA = a0+b0\n if speedUp and totA <= 0 or not speedUp and totA >= 0 then\n return -1, -1 -- no solution\n end\n local distanceToMax, timeToMax = 0, 0\n -- If, the T50 time is set, then assume engine is at zero thrust and will\n -- reach full thrust in 2*T50 seconds. Thrust curve is given by:\n -- Thrust: F(z)=(a0*(1+sin(z))+2*b0)/2 where z=pi*(t/t50 - 1)/2\n -- Acceleration is given by F(z)/m(z) where m(z) = m/sqrt(1-v^2/c^2)\n -- or v(z)' = (a0*(1+sin(z))+2*b0)*sqrt(1-v(z)^2/c^2)/2\n if a0 ~= 0 and t50 > 0 then\n -- Closed form solution for velocity exists:\n -- v(t) = -c*tan(w)/sqrt(tan(w)^2+1) => w = -asin(v/c)\n -- w=(pi*t*(a0/2+b0)-a0*t50*sin(pi*t/2/t50)+*pi*c*k1)/pi/c\n -- @ t=0, v(0) = vi\n -- pi*c*k1/pi/c = -asin(vi/c)\n -- k1 = asin(vi/c)\n local k1 = math.asin(initial/C)\n local c1 = math.pi*(a0/2+b0)\n local c2 = a0*t50\n local c3 = C*math.pi\n local v = function(t)\n local w = (c1*t - c2*math.sin(math.pi*t/2/t50) + c3*k1)/c3\n local tan = math.tan(w)\n return C*tan/math.sqrt(tan*tan+1)\n end\n local speedchk = speedUp and function(s) return s >= final end or\n function(s) return s <= final end\n timeToMax = 2*t50\n if speedchk(v(timeToMax)) then\n local lasttime = 0\n while math.abs(timeToMax - lasttime) > 0.5 do\n local t = (timeToMax + lasttime)/2\n if speedchk(v(t)) then\n timeToMax = t \n else\n lasttime = t\n end\n end\n end\n -- There is no closed form solution for distance in this case.\n -- Numerically integrate for time t=0 to t=2*T50 (or less)\n local lastv = initial\n local tinc = timeToMax/ITERATIONS\n for step = 1, ITERATIONS do\n local speed = v(step*tinc)\n distanceToMax = distanceToMax + (speed+lastv)*tinc/2\n lastv = speed\n end\n if timeToMax < 2*t50 then\n return distanceToMax, timeToMax\n end\n initial = lastv\n end\n -- At full thrust, acceleration only depends on the Lorentz factor:\n -- v(t)' = (F/m(v)) = a*sqrt(1-v(t)^2/c^2) where a = a0+b0\n -- -> v = c*sin((at+k1)/c)\n -- @ t=0, v=vi: k1 = c*asin(vi/c)\n -- -> t = (c*asin(v/c) - k1)/a\n -- x(t)' = c*sin((at+k1)/c)\n -- x = k2 - c^2 cos((at+k1)/c)/a\n -- @ t=0, x=0: k2 = c^2 * cos(k1/c)/a\n local k1 = C*math.asin(initial/C)\n local time = (C * math.asin(final/C) - k1)/totA\n local k2 = C2 *math.cos(k1/C)/totA\n local distance = k2 - C2 * math.cos((totA*time + k1)/C)/totA\n return distance+distanceToMax, time+timeToMax\nend\n--\n-- computeTravelTime - \"relativistic\" version of t=(sqrt(2ad+v^2)-v)/a\n-- initialSpeed [in]: initial (positive) speed in meters per second\n-- acceleration [in]: constant acceleration until 'distance' is traversed\n-- distance [in]: the distance traveled in meters\n-- return: the time in seconds spent in traversing the distance\n--\nfunction Kinematic.computeTravelTime(initial, acceleration, distance)\n -- The low speed limit of following is: t=(sqrt(2ad+v^2)-v)/a\n -- (from: d=vt+at^2/2)\n if distance == 0 then return 0 end\n if acceleration > 0 then\n local k1 = C*math.asin(initial/C)\n local k2 = C2*math.cos(k1/C)/acceleration\n return (C*math.acos(acceleration*(k2 - distance)/C2) - k1)/acceleration\n end\n assert(initial > 0, 'Acceleration and initial speed are both zero.')\n return distance/initial\nend\nfunction Kinematic.lorentz(v) return lorentz(v) end\nreturn Kinematic\nend\nPlanetaryReference = PlanetRef()\ngalaxyReference = PlanetaryReference(Atlas())\nKinematic = Kinematics()\nKep = Keplers()\nfunction getDistanceDisplayString(distance)\n local su = distance > 100000\n local result = \"\"\n if su then\n -- Convert to SU\n result = round(distance/1000/200,1) .. \" SU\"\n else\n -- Convert to KM\n result = round(distance/1000,1) .. \" KM\"\n end\n\n return result\nend\n\nPlanetaryReference = PlanetRef()\ngalaxyReference = PlanetaryReference(Atlas())\n\nMapScreenButtons = {}\nMapScreenMouseX = 0\nMapScreenMouseY = 0\nMapScreenMouseDown = false\nMapScreenButtonSelected = 0\nlocal worldPos = vec3(core.getConstructWorldPos())\nlocal locX = (worldPos.x/400000)\nlocal locY = (worldPos.y/400000)*(-1)\nlocal destX = 0\nlocal destY = 0\nlocal sudistance = 0\nlocal loc = vec3(core.getConstructWorldPos())\nlocal ion = galaxyReference[0][120] ---uses Atlas functions\nlocal thades = vec3(29165536.000, 10865536.000, 65536.000)\nlocal sinnen = vec3(58665536.000, 29665536.000, 58165536.000)\nlocal alioth = galaxyReference[0][2] ---uses Atlas functions\nlocal madis = vec3(17465536.000, 22665536.000, -34464.000)\nlocal jago = vec3(-94134464.000, 12765536.000, -3634464.000)\nlocal symeon = vec3(14165536.000, -85634464.000, -934464.000)\nlocal lacobus = vec3(98865536.000, -13534464.000, -934464.000)\nlocal teoma = vec3(80865536.000, 54665536.000, -934464.000)\nlocal feli = vec3(-43534464.000, 22565536.000, -48934464.000)\nlocal talemai = vec3(-13234464.000, 55765536.000, 465536.000)\nlocal sicari = vec3(52765536.000, 27165536.000, 52065536.000)\nlocal distion = math.floor(ion:getDistance(loc)/200000) ---uses getDistance functions----\nlocal distthades = string.format(\"%.2f\", math.sqrt((loc.x-thades.x)^2+(loc.y-thades.y)^2+(loc.z-thades.z)^2)/200000)\nlocal distalioth = math.floor(alioth:getDistance(loc)/200000) ---uses getDistance functions----\nlocal distmadis = string.format(\"%.2f\", math.sqrt((loc.x-madis.x)^2+(loc.y-madis.y)^2+(loc.z-madis.z)^2)/200000)\nlocal distjago = string.format(\"%.2f\", math.sqrt((loc.x-jago.x)^2+(loc.y-jago.y)^2+(loc.z-jago.z)^2)/200000)\nlocal distlacobus = string.format(\"%.2f\", math.sqrt((loc.x-lacobus.x)^2+(loc.y-lacobus.y)^2+(loc.z-lacobus.z)^2)/200000)\nlocal distteoma = string.format(\"%.2f\", math.sqrt((loc.x-teoma.x)^2+(loc.y-teoma.y)^2+(loc.z-teoma.z)^2)/200000)\nlocal distsymeon = string.format(\"%.2f\", math.sqrt((loc.x-symeon.x)^2+(loc.y-symeon.y)^2+(loc.z-symeon.z)^2)/200000)\nlocal distfeli = string.format(\"%.2f\", math.sqrt((loc.x-feli.x)^2+(loc.y-feli.y)^2+(loc.z-feli.z)^2)/200000)\nlocal distsinnen = string.format(\"%.2f\", math.sqrt((loc.x-sinnen.x)^2+(loc.y-sinnen.y)^2+(loc.z-sinnen.z)^2)/200000)\nlocal disttalemai = string.format(\"%.2f\", math.sqrt((loc.x-talemai.x)^2+(loc.y-talemai.y)^2+(loc.z-talemai.z)^2)/200000)\nlocal distsicari = string.format(\"%.2f\", math.sqrt((loc.x-sicari.x)^2+(loc.y-sicari.y)^2+(loc.z-sicari.z)^2)/200000)\n\n\n\n for i = 1,1 do\n local button = {id = (\"b\"..1), enabled=true, td=\"<td>\", top=2/100, bottom=13/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 2,2 do\n local button = {id = (\"b\"..2), enabled=true, td=\"<td>\", top=15/100, bottom=26/100, left=1/100, right=30/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 3,3 do\n local button = {id = (\"b\"..3), enabled=true, td=\"<td>\", top=27/100, bottom=38/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 4,4 do \n local button = {id = (\"b\"..4), enabled=true, td=\"<td>\", top=39/100, bottom=50/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 5,5 do \n local button = {id = (\"b\"..5), enabled=true, td=\"<td>\", top=51/100, bottom=62/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 6,6 do \n local button = {id = (\"b\"..6), enabled=true, td=\"<td>\", top=64/100, bottom=75/100, left=1/100, right=28/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 7,7 do \n local button = {id = (\"b\"..7), enabled=true, td=\"<td>\", top=2/100, bottom=13/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 8,8 do \n local button = {id = (\"b\"..8), enabled=true, td=\"<td>\", top=15/100, bottom=26/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 9,9 do \n local button = {id = (\"b\"..9), enabled=true, td=\"<td>\", top=27/100, bottom=38/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 10,10 do \n local button = {id = (\"b\"..10), enabled=true, td=\"<td>\", top=39/100, bottom=50/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 11,11 do \n local button = {id = (\"b\"..11), enabled=true, td=\"<td>\", top=51/100, bottom=62/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 12,12 do \n local button = {id = (\"b\"..12), enabled=true, td=\"<td>\", top=64/100, bottom=75/100, left=75/100, right=100/100}\n table.insert(MapScreenButtons, button)\nend\n for i = 13,13 do \n local button = {id = (\"b\"..13), enabled=true, td=\"<td>\", top=90/100, bottom=100/100, left=1/100, right=18/100}\n table.insert(MapScreenButtons, button)\nend\nfunction evaluateButtons()\n local selected = 0\n \n if #MapScreenButtons >= 1 then\n -- Set button styles\n for i, button in ipairs(MapScreenButtons) do\n if button.left < MapScreenMouseX and MapScreenMouseX < button.right and button.top < MapScreenMouseY and MapScreenMouseY < button.bottom then\n if MapScreenMouseDown and MapScreenButtonSelected == i then\n end\n selected = i\n end\n if not button.enabled then\n end\n\n end\n end\n return selected\nend\n\nfunction onButtonDown(buttonNo)\n local button = MapScreenButtons[buttonNo] \n if not button or not button.enabled then\n\treturn\n end\nend\nfunction onButtonUp(buttonNo)\n local button = MapScreenButtons[buttonNo] \n if not button or not button.enabled then\n return\n end\nfunction onClick(buttonNo)\n local button = MapScreenButtons[buttonNo] \n if not button or not button.enabled then\n return\n end\nend\n if buttonNo == 1 then\ndestX = 0\ndestY = 0\nsudistance = distalioth\n elseif buttonNo == 2 then\ndestX = 43\ndestY = -56\nsudistance = distmadis\n elseif buttonNo == 3 then\ndestX = 73\ndestY = -27\nsudistance = distthades \n elseif buttonNo == 4 then\ndestX = -33\ndestY = -139\nsudistance = disttalemai\n elseif buttonNo == 5 then\ndestX = -109\ndestY = -56\nsudistance = distfeli \n elseif buttonNo == 6 then\ndestX = 131\ndestY = -68\nsudistance = distsicari \n elseif buttonNo == 7 then\ndestX = 35\ndestY = 214\nsudistance = distsymeon\n elseif buttonNo == 8 then\ndestX = 146\ndestY = -74\nsudistance = distsinnen \n elseif buttonNo == 9 then\ndestX = -235\ndestY = -32\nsudistance = distjago \n elseif buttonNo == 10 then\ndestX = 202\ndestY = -137\nsudistance = distteoma \n elseif buttonNo == 11 then\ndestX = 7\ndestY = 247\nsudistance = distion \n elseif buttonNo == 12 then\ndestX = 247\ndestY = 34\nsudistance = distlacobus\n elseif buttonNo == 13 then\n unit.exit()\n end\nend\n\nfunction updateScreen() \nwarpmath = math.floor(math.floor(core.getConstructMass()/ 1000) * sudistance * 0.00025)\nhtml= ([[\n<svg class=\"bootstrap\" viewBox=\"0 0 1024 1024\" style=\"width:100%; height:100%\"><circle cx=\"500\" cy=\"500\" r=\"400\" stroke=\"darkgreen\" stroke-width=\"3\" transform=\"\"></circle><circle cx=\"500\" cy=\"500\" r=\"350\" stroke=\"darkgreen\" stroke-width=\"3\" transform=\"\" stroke-opacity=\"0.2\"></circle><circle cx=\"500\" cy=\"500\" r=\"300\" stroke=\"darkgreen\" stroke-width=\"3\" transform=\"\"></circle><circle cx=\"500\" cy=\"500\" r=\"250\" stroke=\"darkgreen\" stroke-width=\"3\" transform=\"\" stroke-opacity=\"0.2\"></circle><circle cx=\"500\" cy=\"500\" r=\"200\" stroke=\"darkgreen\" stroke-width=\"3\" transform=\"\"></circle><circle cx=\"500\" cy=\"500\" r=\"150\" stroke=\"darkgreen\" stroke-width=\"3\" transform=\"\" stroke-opacity=\"0.2\"></circle><circle cx=\"500\" cy=\"500\" r=\"100\" stroke=\"lightblue\" stroke-width=\"3\" transform=\"\"></circle><circle cx=\"500\" cy=\"500\" r=\"50\" stroke=\"lightblue\" stroke-width=\"3\" transform=\"\" stroke-opacity=\"0.2\"></circle><circle cx=\"500\" cy=\"500\" r=\"20\" stroke=\"Orange\" stroke-width=\"2\" transform=\"\"></circle><text x=\"510\" y=\"510\" fill=\"Yellow\">Helios</text><circle cx=\"-0.00\" cy=\"0\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"-0.00\" y=\"0\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Alioth</text><circle cx=\"7.16\" cy=\"247.59\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"7.16\" y=\"247.59\" transform=\"translate(480,480)\" fill=\"white\" font-size=\"20\">Ion</text><circle cx=\"35.41\" cy=\"214.09\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"35.41\" y=\"214.09\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Symeon</text><circle cx=\"-33.09\" cy=\"-139.41\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"-33.09\" y=\"-139.41\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Talemai</text><circle cx=\"202.16\" cy=\"-136.66\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"202.16\" y=\"-136.66\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Teoma</text><circle cx=\"247.16\" cy=\"33.84\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"247.16\" y=\"33.84\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Lacobus</text><circle cx=\"-108.84\" cy=\"-56.41\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"-108.84\" y=\"-56.41\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Feli</text><circle cx=\"72.91\" cy=\"-27.16\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"72.91\" y=\"-27.16\" transform=\"translate(500,485)\" fill=\"white\" font-size=\"20\">Thades</text><circle cx=\"43.66\" cy=\"-56.66\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"43.66\" y=\"-56.66\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Madis</text><circle cx=\"-235.34\" cy=\"-31.91\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"-235.34\" y=\"-31.91\" transform=\"translate(500,480)\" fill=\"white\" font-size=\"20\">Jago</text><circle cx=\"131.91\" cy=\"-67.91\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"131.91\" y=\"-67.91\" transform=\"translate(475,480)\" fill=\"white\" font-size=\"20\">Sicari</text><circle cx=\"146.66\" cy=\"-74.16\" r=\"10\" stroke=\"black\" stroke-width=\"1\" fill=\"blue\" transform=\"translate(500,500)\"></circle><text x=\"146.66\" y=\"-74.16\" transform=\"translate(515,480)\" fill=\"white\" font-size=\"20\">Sinnen</text>\n<line stroke-linecap=\"undefined\" stroke-linejoin=\"undefined\" id=\"svg_1\" y2=\"]]..destY..[[\" x2=\"]]..destX..[[\" y1=\"]]..locY..[[\" x1=\"]]..locX..[[\" transform=\"translate(500,500)\" stroke-width=\"5\" stroke=\"#ff0000\" fill=\"none\"/> \n<circle cx=\"]]..locX..[[\" cy=\"]]..locY..[[\" r=\"3\" stroke=\"black\" stroke-width=\"1\" fill=\"limegreen\" transform=\"translate(500,500)\"></circle>\n<text x=\"]]..locX..[[\" y=\"]]..locY..[[\" transform=\"translate(500,500)\" \nfill=\"limegreen\" font-size= \"4.5vh\" font-weight= \"bold\">//SHIP POSITION</text>\n</svg>\n<svg class=\"bootstrap\" viewBox=\"0 0 1024 612\" style=\"width:100%; height:100%\">\n <g>\n <title>Layer 1</title>\n <g id=\"svg_24\">\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_8\" y=\"70\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Alioth :]]..distalioth..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_14\" y=\"170\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Madis :]]..distmadis..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_17\" y=\"270\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Thades :]]..distthades..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_20\" y=\"370\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Talemai :]]..disttalemai..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_23\" y=\"470\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Feli :]]..distfeli..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_26\" y=\"570\" x=\"55\" stroke-width=\"0\" fill=\"Yellow\">Sicari :]]..distsicari..[[ SU</text>\n <g id=\"svg_12\">\n <rect rx=\"10\" id=\"svg_1\" height=\"50\" width=\"250\" y=\"30\" x=\"15\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_3\" height=\"50\" width=\"250\" y=\"105\" x=\"15\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_7\" height=\"50\" width=\"250\" y=\"180\" x=\"15\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_9\" height=\"50\" width=\"250\" y=\"255\" x=\"15\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_10\" height=\"50\" width=\"250\" y=\"330\" x=\"15\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_11\" height=\"50\" width=\"250\" y=\"405\" x=\"15\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n </g>\n </g>\n <g id=\"svg_40\">\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_25\" y=\"70\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Symeon :]]..distsymeon..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_27\" y=\"170\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Sinnen :]]..distsinnen..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_28\" y=\"270\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Jago :]]..distjago..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_30\" y=\"370\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Teoma :]]..distteoma..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_31\" y=\"470\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Ion :]]..distion..[[ SU</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"20\" id=\"svg_32\" y=\"570\" x=\"997.163642\" stroke-width=\"0\" fill=\"Yellow\">Lacobus :]]..distlacobus..[[ SU</text>\n <g id=\"svg_39\">\n <rect rx=\"10\" id=\"svg_33\" height=\"50\" width=\"250\" y=\"30\" x=\"760\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_34\" height=\"50\" width=\"250\" y=\"105\" x=\"760\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_35\" height=\"50\" width=\"250\" y=\"180\" x=\"760\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_36\" height=\"50\" width=\"250\" y=\"255\" x=\"760\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_37\" height=\"50\" width=\"250\" y=\"330\" x=\"760\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n <rect rx=\"10\" id=\"svg_38\" height=\"50\" width=\"250\" y=\"405\" x=\"760\" stroke-width=\"20\" stroke=\"#00ff00\" fill=\"none\"/>\n </g>\n </g>\n </g>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"30\" id=\"svg_32\" y=\"700\" x=\"20\" stroke-width=\"0\" fill=\"LightBlue\">Est. Warp Cost: ]]..warpmath..[[</text>\n <text stroke=\"null\" transform=\"matrix(0.7907331239400577,0,0,0.7600725676692406,3.135703637258853,5.731969683147472) \" xml:space=\"preserve\" text-anchor=\"start\" font-family=\"Helvetica, Arial, sans-serif\" font-size=\"30\" id=\"svg_32\" y=\"750\" x=\"20\" stroke-width=\"0\" fill=\"LightBlue\">Construct Weight: ]]..math.floor(core.getConstructMass()/ 1000)..[[ tons</text>\n \n</svg> \n ]])\nscreen.setHTML(html)\nend\nunit.setTimer(\"spacemap\",.08)\n\n\n","filter":{"args":[],"signature":"start()","slotKey":"-1"},"key":"2"},{"code":"updateScreen()","filter":{"args":[{"value":"spacemap"}],"signature":"tick(timerId)","slotKey":"-1"},"key":"3"}],"methods":[],"events":[]}
Hello all Noveans,
So ive made a small program that i call Screen++ that enables you to add animations to your screens easily. You can use it to create geometrical shapes like ovals, circles or lines and animate them. You can make the geometrical shapes to move in x or y coordinate or change the colors of the border och background of the shapes in intervalls. You can add text and animate them the same way you can animate the geometrical shapes. Check out the newest version (below) to see what new features has been added.
-------------------------------------------------------------------- NEW VERSION 3.0 -------------------------------------------------------------------- DATE: 2020 11TH OCTOBER
--NEW in version 3.0:
-- added ability to set background image, import any picture you like and display it on your screen, normal (use base64)
-- +/- in displace elemets in all direction
-- added rotation for all functions, clockwise or counter clockwise
-- added triangle, normal and animated
-- added rectangle, normal and animated (square, width=height)
-- added ability to set backgroundcolor, normal and animated
-- Z-index, whats elements that should be behind or infront of other elements
-- added so all functions can have filled or transparent background (only border will show)
-- possible to use Hexcolors
-- use variables
-- link code/animations to external elements (like a door for example)
Tutorial on how to use Screen++ 3.0:
I STRONGLY recommend that you watch the video on youtube and not here. Because ive putted timestamps so you easier can navigate through the video
This is the link to the codes that you need to copy and past into your programming board (github):
https://github.com/robarzangana/dualuniverseRepo/blob/main/screenplusplus_version_3.0
If you have any questions/requests be sure to tell me about them here or on youtube.
I hope you'll enjoy it!
-------------------------------------------------------------------- OLD VERSION 2.0 --------------------------------------------------------------------
Ive made a tutorial on youtube on how to use Screen++, and im sorry in advance, because i mess up few times in the video. (its my second video):
This is the link to the codes that you need to copy and past into your programming board (github): https://github.com/robarzangana/dualuniverseRepo/blob/main/screenplusplus_version_2.0
If you have any questions/requests be sure to tell me about them here or on youtube.
I hope you'll enjoy it!
Requires
3 Programming Boards
2 Databanks --two is needed to prevent weird code crossing bugs. later this may be less when they fix bug.
20 Containers of same Size
1 screen
1 switch
1 relay
PB1->switch-> relay-> PB2 PB3
Create Events in Lua Editor and Paste the Following as Instructed.
9/17 - Fixed parameter for single boards.Changed some names and Added more exports
Programming Board 1 -- Can do 9 Containers OR Read from Databanks
---screen
---databank-----only if your doing more than 9 items added last
---databank2-----only if your doing more than 9 items(using 2 helps code from being crossed from bugs)added last
---switch-----only if your doing more than 9 items
----Unit Start
if Morethan9slots == "On" then
switch.activate()
end
unit.setTimer("Live",1)
unit.hide()
----Unit Tick ---Name the Tick Live
Morethan9slots = "Off" --export:Off for 9 slots and On for more than 9 and requires databanks.
local containermax = 9600 --export:;Your max container holding.
local slot1item = "Bauxite" --export:;Slot1 Iten.
local slot1weight = 1.28 --export:;Slot1 weight.
local slot2item = "Coal" --export:;Slot2 Iten.
local slot2weight = 1.35 --export:;Slot2 weight.
local slot3item = "Hematite" --export:;Slot3 Iten.
local slot3weight = 5.04 --export:;Slot3 weight.
local slot4item = "Quartz" --export:;Slot4 Iten.
local slot4weight = 2.65 --export:;Slot4 weight.
local slot5item = "Chromite" --export:;Slot5 Iten.
local slot5weight = 4.54 --export:;Slot5 weight.
local slot6item = "Limestone" --export:;Slot6 Iten.
local slot6weight = 2.71 --export:;Slot6 weight.
local slot7item = "Malachite" --export:;Slot7 Iten.
local slot7weight = 4.0 --export:;Slot7 weight.
local slot8item = "Natron" --export:;Slot8 Iten.
local slot8weight = 1.55 --export:;Slot8 weight.
local slot9item = "Acanthite" --export:;Slot9 Iten.
local slot9weight = 7.2 --export:;Slot9 weight.
if Morethan9slots == "Off" then
local dbhtml = ""
local dhtml = ""
local index = {1, 2, 3, 4, 5, 6, 7, 8, 9} -- Row of Container?
local containers = {slot1, slot2, slot3, slot4, slot5, slot6, slot7, slot8, slot9} -- slot names
local weights = {slot1weight, slot2weight, slot3weight, slot4weight, slot5weight, slot6weight, slot7weight, slot8weight, slot9weight} -- inspected kg of item
local items = {slot1item, slot2item, slot3item, slot4item, slot5item, slot6item, slot7item, slot8item, slot9item} -- names to display
local htmlContent = ""
for i=1, #containers do
htmlContent = htmlContent .. "<tr>".."<th>"..index[i].."</th><th>"..items[i].."</th><th>"..math.ceil(((math.ceil((containers[i].getItemsMass()/weights[i]) - 0.5)/containermax)*100)).."%</th><th>"..math.ceil((containers[i].getItemsMass()/weights[i]) - 0.5).."</th><tr>"
end
local html = [[
<table style="
margin-left: auto;
margin-right: auto;
width:30%;
font-size:1.25em;
text-align:left;">
<tr style = "
background-color:Purple;
color:black !important;">
<svg>
<g>
<text xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="30" id="svg_8" y="50" x="10" stroke="#ff0000" fill="#ff7f00">PB1</text>
</g></svg>
<th>Row</th>
<th>Product</th>
<th>Container%</th>
<th>Total Ore</th>
</tr>
]]..htmlContent..[[
</table>]]
screen.setHTML(html)
elseif Morethan9slots == "On" then
switch.activate()
dbhtml = databank.getStringValue(OreMonitorTwo)
dhtml = databank2.getStringValue(OreMonitorThree)
local index = {1, 2, 3, 4, 5, 6} -- Row of Container?
local containers = {slot1, slot2, slot3, slot4, slot5, slot6} -- slot names
local weights = {slot1weight, slot2weight, slot3weight, slot4weight, slot5weight, slot6weight} -- inspected kg of item
local items = {slot1item, slot2item, slot3item, slot4item, slot5item, slot6item} -- names to display
local htmlContent = ""
for i=1, #containers do
htmlContent = htmlContent .. "<tr>".."<th>"..index[i].."</th><th>"..items[i].."</th><th>"..math.ceil(((math.ceil((containers[i].getItemsMass()/weights[i]) - 0.5)/containermax)*100)).."%</th><th>"..math.ceil((containers[i].getItemsMass()/weights[i]) - 0.5).."</th><tr>"
end
local html = [[
<table style="
margin-left: auto;
margin-right: auto;
width:30%;
font-size:1.25em;
text-align:left;">
<tr style = "
background-color:Purple;
color:black !important;">
<svg>
<g>
<text xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="30" id="svg_8" y="50" x="10" stroke="#ff0000" fill="#ff7f00">PB1</text>
</g></svg>
<th>Row</th>
<th>Product</th>
<th>Container%</th>
<th>Total Ore</th>
</tr>
]]..htmlContent..[[]]..dbhtml..[[]]..dhtml..[[
</table>]]
screen.setHTML(html)
end
---Unit Stop
if Morethan9slots == "On" then
switch.deactivate()
end
screen.clear()
Programming Board 2
--databank is last slot to add and named databank
---Unit Start
unit.setTimer("Live",1)
unit.hide()
----Unit Tick ---Name the Tick Live
--databank is last slot to add and named databank
local slot1item = "Malachite" --export:;Slot1 Iten.
local slot1weight = 4.0 --export:;Slot1 weight.
local slot2item = "Natron" --export:;Slot2 Iten.
local slot2weight = 1.55 --export:;Slot2 weight.
local slot3item = "Acanthite" --export:;Slot3 Iten.
local slot3weight = 7.2 --export:;Slot3 weight.
local slot4item = "Garnierite" --export:;Slot4 Iten.
local slot4weight = 2.60 --export:;Slot4 weight.
local slot5item = "Petalite" --export:;Slot5 Iten.
local slot5weight = 2.41 --export:;Slot5 weight.
local slot6item = "Pyrite" --export:;Slot6 Iten.
local slot6weight = 5.01 --export:;Slot6 weight.
local slot7item = "Colbaltite" --export:;Slot7 Iten.
local slot7weight = 6.33 --export:;Slot7 weight.
local slot8item = "Cryolite" --export:;Slot8 Iten.
local slot8weight = 2.95 --export:;Slot8 weight.
local slot9item = "Gold Nuggets" --export:;Slot9 Iten.
local slot9weight = 19.30 --export:;Slot9 weight.
local dbhtml = ""
local dhtml = ""
local index = {7, 8, 9, 10, 11, 12, 13, 14, 15} -- Row of Container?
local containers = {slot1, slot2, slot3, slot4, slot5, slot6, slot7, slot8, slot9} -- slot names
local weights = {slot1weight, slot2weight, slot3weight, slot4weight, slot5weight, slot6weight, slot7weight, slot8weight, slot9weight} -- inspected kg of item
local items = {slot1item, slot2item, slot3item, slot4item, slot5item, slot6item, slot7item, slot8item, slot9item} -- names to display
local htmlContent = ""
local containermax = 9600 --export:;Your max container holding.
for i=1, #containers do
htmlContent = htmlContent .. "<tr>".."<th>"..index[i].."</th><th>"..items[i].."</th><th>"..math.ceil(((math.ceil((containers[i].getItemsMass()/weights[i]) - 0.5)/containermax)*100)).."%</th><th>"..math.ceil((containers[i].getItemsMass()/weights[i]) - 0.5).."</th><tr>"
end
local html = [[
<table style="
margin-left: auto;
margin-right: auto;
width:30%;
font-size:1.25em;
text-align:left;">
<tr style = "
background-color:Purple;
color:black !important;">
<svg>
<g>
<text xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="30" id="svg_8" y="50" x="10" stroke="#ff0000" fill="#ff7f00">PB2</text>
</g></svg>
<th>Row</th>
<th>Product</th>
<th>Container%</th>
<th>Total Ore</th>
</tr>
]]..htmlContent..[[
</table>]]
databank.setStringValue(OreMonitorTwo,html)
Programming Board 3
--databank is last slot to add and named databank
---Unit Start
unit.setTimer("Live",1)
unit.hide()
----Unit Tick ---Name the Tick Live
--databank is last slot to add and named databank
local slot1item = "Kobelckite" --export:;Slot1 Iten.
local slot1weight = 2.37 --export:;Slot1 weight.
local slot2item = "Columbite" --export:;Slot2 Iten.
local slot2weight = 5.38 --export:;Slot2 weight.
local slot3item = "Illmenite" --export:;Slot3 Iten.
local slot3weight = 4.55 --export:;Slot3 weight.
local slot4item = "Rhodonite" --export:;Slot4 Iten.
local slot4weight = 3.76 --export:;Slot4 weight.
local slot5item = "Vanadinite" --export:;Slot5 Iten.
local slot5weight = 6.95 --export:;Slot5 weight.
local slot6item = "Not set" --export:;Slot6 Iten.
local slot6weight = 0 --export:;Slot6 weight.
local slot7item = "Not set" --export:;Slot7 Iten.
local slot7weight = 0 --export:;Slot7 weight.
local slot8item = "Not set" --export:;Slot8 Iten.
local slot8weight = 0 --export:;Slot8 weight.
local slot9item = "Not set" --export:;Slot9 Iten.
local slot9weight = 0 --export:;Slot9 weight.
local index = {16, 17, 18, 19, 20} -- Row of Container?
local containers = {slot1, slot2, slot3, slot4, slot5, slot6, slot7, slot8, slot9} -- slot names
local weights = {slot1weight, slot2weight, slot3weight, slot4weight, slot5weight, slot6weight, slot7weight, slot8weight, slot9weight} -- inspected kg of item
local items = {slot1item, slot2item, slot3item, slot4item, slot5item, slot6item, slot7item, slot8item, slot9item} -- names to display
local htmlContent = ""
local containermax = 1200 --export:;Your max container holding.
for i=1, #containers do
htmlContent = htmlContent .. "<tr>".."<th>"..index[i].."</th><th>"..items[i].."</th><th>"..math.ceil(((math.ceil((containers[i].getItemsMass()/weights[i]) - 0.5)/containermax)*100)).."%</th><th>"..math.ceil((containers[i].getItemsMass()/weights[i]) - 0.5).."</th><tr>"
end
local html = [[
<table style="
margin-left: auto;
margin-right: auto;
width:30%;
font-size:1.25em;
text-align:left;">
<tr style = "
background-color:Purple;
color:black !important;">
<svg>
<g>
<text xml:space="preserve" text-anchor="start" font-family="Helvetica, Arial, sans-serif" font-size="30" id="svg_8" y="50" x="10" stroke="#ff0000" fill="#ff7f00">PB3</text>
</g></svg>
<th>Row</th>
<th>Product</th>
<th>Container%</th>
<th>Total Ore</th>
</tr>
]]..htmlContent..[[
</table>]]
databank.setStringValue(OreMonitorThree,html)
Well topically this thread is incorrect. Mechanically I am of two minds - one, yeah it sucks to have your ship moved without your consent to PvP space and destroyed. However, the mechanics used to do this are sound. Why, do you ask, easy:
1) You want players to remove junk from their property. So we don't want the ability to remove constructs from your land as that just means folks will grief you by parking borg cubes on your ship/base so you can't use it.
2) You want players to be able to tow other player's ships (as a "business" or as an "org function" or something similar). This is immersive and potential gameplay - AAA ship transport and towing.
3) You were offline but 1 and 2 still need to be viable as not having them would allow worse things to happen or not allow emergent gameplay
I don't see folks complaining about people free range mining land they haven't claimed.
I don't see folks complaining about people putting borg shells over their property as a "denial of use" effort.
Yes it sucks, yes it's a lesson for us all, but no, as the game mechanics were used and you did park your ship at an insecure location and it got stolen, it is not an exploit. Sadly I can't agree with the OP no matter how much I want to agree with the OP.
Well topically this thread is incorrect. Mechanically I am of two minds - one, yeah it sucks to have your ship moved without your consent to PvP space and destroyed. However, the mechanics used to do this are sound. Why, do you ask, easy:
1) You want players to remove junk from their property. So we don't want the ability to remove constructs from your land as that just means folks will grief you by parking borg cubes on your ship/base so you can't use it.
2) You want players to be able to tow other player's ships (as a "business" or as an "org function" or something similar). This is immersive and potential gameplay - AAA ship transport and towing.
3) You were offline but 1 and 2 still need to be viable as not having them would allow worse things to happen or not allow emergent gameplay
I don't see folks complaining about people free range mining land they haven't claimed.
I don't see folks complaining about people putting borg shells over their property as a "denial of use" effort.
Yes it sucks, yes it's a lesson for us all, but no, as the game mechanics were used and you did park your ship at an insecure location and it got stolen, it is not an exploit. Sadly I can't agree with the OP no matter how much I want to agree with the OP.
Bluntly based on the lore of the game no pirates would have made the trip. I mean they would send the best people from Earth if they had to send anyone and people whose sole ambition in life is to steal other peoples stuff just wouldn't have been allowed near the ark ships period. So lore-wise pirates based on the colonist sent to out should not exist. There's no lore to support them at all as all pirates would have been the first to get burned alive when Earth blew up or what not.
Knowing humans and how they think I am pretty sure lore-wise Earth would have sent an existing government entity to help settle the colony and police it. Who else built all the markets - those government folks sent to run the colonies.
Where PvP should exist is between Organizations which would have people actively supporting their beliefs in the direction the new colonies should go. So PvP should exist but only between Org members and only during Org sanctioned events mainly due to a FFA would bring the ire of the colony government and offending parties would be banned from the markets - easy enough, the offender's claims would be relinquished because humans like to take "bad guy's" things, and their rep would be at a point where if they showed up armed in colony space they'd be reacted to as a criminal threat.
So lore-wise PvP should be an exception and not a FFA affair. The current state of PvP is an offence against the current lore.
Bluntly based on the lore of the game no pirates would have made the trip. I mean they would send the best people from Earth if they had to send anyone and people whose sole ambition in life is to steal other peoples stuff just wouldn't have been allowed near the ark ships period. So lore-wise pirates based on the colonist sent to out should not exist. There's no lore to support them at all as all pirates would have been the first to get burned alive when Earth blew up or what not.
Knowing humans and how they think I am pretty sure lore-wise Earth would have sent an existing government entity to help settle the colony and police it. Who else built all the markets - those government folks sent to run the colonies.
Where PvP should exist is between Organizations which would have people actively supporting their beliefs in the direction the new colonies should go. So PvP should exist but only between Org members and only during Org sanctioned events mainly due to a FFA would bring the ire of the colony government and offending parties would be banned from the markets - easy enough, the offender's claims would be relinquished because humans like to take "bad guy's" things, and their rep would be at a point where if they showed up armed in colony space they'd be reacted to as a criminal threat.
So lore-wise PvP should be an exception and not a FFA affair. The current state of PvP is an offence against the current lore.
I don't know about you but I don't want to spend 2-3 weeks building an at most medium transport only to be ganked by someone who only specs PvP ships. Yay, so you spent a month logging into the game to get your free credits and adjust your unattended talent tree. That shouldn't be a free ticket to gank everyone who actually puts effort and time into building something, and you know, actually plays the game to build their stuff vice camping out and buying a market fighter...
Just saying. I'd be happy with a "New World" type PvP system where orgs can battle it out for control of planets during declared war periods.
I don't know about you but I don't want to spend 2-3 weeks building an at most medium transport only to be ganked by someone who only specs PvP ships. Yay, so you spent a month logging into the game to get your free credits and adjust your unattended talent tree. That shouldn't be a free ticket to gank everyone who actually puts effort and time into building something, and you know, actually plays the game to build their stuff vice camping out and buying a market fighter...
Just saying. I'd be happy with a "New World" type PvP system where orgs can battle it out for control of planets during declared war periods.
With Beta now out for several weeks, I have been inundated with requests about my simple way to plan factory production lines, that I had shown off during the games Alpha.
Needless to say, since the Beta release, I have been hard at work as a Community Helper and also as the Super Legate of my Guild. But alas, I have finally found some free time to sit down and share a way to make the Industry designing of DU go from Hellish to Simple!
First off:
Firstly I just want to say that this method I will be sharing does NOT replace building calculators, but instead works in tangent with them. A crafting calculator may well tell you all the numbers you need, but it doesn't help organise it all. That is where this will come in to play.
Also it is important that I credit Juvenious, who initially inspired me to make this and showcase it off in Alpha, which garnered more attention than I ever thought possible, and would like to thank him for his encouragement and help in laying out the ground work. Be sure to visit his Discord *HERE* where he is collecting / making up further standards to help simplify tasks.
So what is it?
The idea was to create a unique set of shapes, that represent one of the industrial factory units in the game, whilst keeping them simple, elegant and familiar in some way to their related task. Then they are placed into a Legend, something that shows you their representation, along with other information as how to interpret the diagrams fully and easily.
In essence, we get this, the SL Factory Standard Legend:
As you can see, a lot of the shapes will either look like a basic silhouette of the industry unit they represent or have some other relation to their purpose. The colour coding is also a massive addition to helping keep things simple, as it then allows you to categorise the industrial units together, helping you keep track of the production line in game, with the colours & their order chosen to mimic that of popular MMO games item grades.
* Please note: The Tier system for the Standard is different to that of the one shown in game. Simply put, the differences are: - In DU, the level of components and subcomponents is broken down into: Intermediary -> Complex -> Functional -> Exceptional. With there being Basic, Uncommon, Advanced, Rare & Exotic tiers.
- In the Standard, it is broken down simply by what the requirements are of the component. i.e. Al-Fe Alloy would be Tier 1, as it requires just Pure to make, which is Tier 0. A Warp Cell would be Tier 5, as the highest tier subcomponent needed to make them, is a Tier 4. Basic, Uncommon etc can be seen as a Grade of item, but does not hold any weight in the Legend or diagrams.
This is all very well, but how can I get it?
So to get started, you will want to head over to https://diagrams.net which is completely free and does not need an account. All your documents are saved in real time, to your Google Drive.
The other thing you will need is a copy of the Standard Legend I have created. Luckily, I can easily share this with you on here through an XML file that can be imported into the website, allowing you full access to all the shapes and their formatting that I use. The Legend has gone under several updates already and may change to improve functionality so do keep checking back.
SL Standard 1.5.xml
* There is currently an issue with downloading attachments on Forums. You can PM me or visit: Novean Institute of Standards discord Planet DU
To upload the XML file, you will want to follow this image below:
(Please note: Select Device if you downloaded the XML file)
This is all great, but how do you use it, exactly?
Once you have the XML file uploaded, a blank page waiting for you to start populating, the next thing you're going to want to do is start putting down the relevant icons needed for each individual, unique blueprint that is required, and group them into the Tier colouring system. Once this is done, simply link the icons together, to show where they need to feed into.
This may sound simple... But it could still be absolutely hell, with a plate of spaghetti in the middle. So here's an example:
So as you can see above, this is how anyone without talents would want to make TCUs for themselves. For individuals, you could simply remove one of the Assembly Line M units and half the numbers to be able to make 1 TCU for your personal endeavours.
There are some simple, but profound guidelines I follow when making diagrams which I can share with you. These are:
1) Never cross over any lines. If you find yourself boxed in, put the supply in later on, with the containers name for reference to the source. i.e. "Tier 1C" 2) Ensure that your lines always feed from left to right. This will stop any confusion in what is feeding into where. An exception can be seen in the image above, where a feed is coming from Tier 3A, up and looping into the Uncommon Power Transformer, which is fine as the only other connections its joining onto are from other containers, which a container cannot feed into another container without the help of a transfer unit. And we can see there is no transfer unit on the diagram. 3) Always name your containers and keep track of how many links they need to output to. If you find you are over the limit of 10 links out, look into either splitting up your base production to feed into a 2nd container, use a transfer unit for a 2nd container and/or increase your talents to reduce the build times, resulting in needing less industry units for efficiency.
So? What are you waiting for? Get drawing!
Practice makes perfect, after all And speaking of such, if you have any feedback or issues with this post, the XML file itself or have any other concerns or questions, please post them here without reservation!
BaconofWar got a reaction from Ravenmoor in These tax rates are absurd.
BaconofWar got a reaction from kulkija in These tax rates are absurd.
BaconofWar got a reaction from DreamAngelCore in [Suggestion] Clear Talent Queue Button
BaconofWar got a reaction from Daphne Jones in [Suggestion] Clear Talent Queue Button
BaconofWar got a reaction from GraXXoR in PVP possible in "Safe Zone"
BaconofWar got a reaction from Supermega in PvP is Broken aka Pay to Win
BaconofWar got a reaction from Anopheles in PVP possible in "Safe Zone"
BaconofWar got a reaction from Moosegun in PVP possible in "Safe Zone"
BaconofWar got a reaction from CptLoRes in PVP VS NON PVP
BaconofWar got a reaction from FryingDoom in When will the space safe zone be removed?
BaconofWar got a reaction from Megaddd in Industry Planning Simplified!