Difference between revisions of "Lua Script for Orbit Stabilization"
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+ | Lua script for chapter 2 of [[Go Play In Space]] by Bruce Irving, Andy McSorley, and Mark Paton for [[Orbiter|Orbiter Space Flight Simulator]]. | ||
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+ | [[Category: Articles]] | ||
[[Category: Lua]] | [[Category: Lua]] |
Latest revision as of 16:02, 14 October 2022
Lua script for chapter 2 of Go Play In Space by Bruce Irving, Andy McSorley, and Mark Paton for Orbiter Space Flight Simulator.
-- Lua script for chapter 2 of "Go Play in Space" - Orbit Stabilization -- -- Author: David Murley -- Date: 7/01/2019 -- Version: 1.1 -- -- term.out('Script invoked') -- Get access to the Delta Gliders GL-01 and GL-02. With the interface handles -- obtained, access to various controls and flight data are acquired. hGL1=vessel.get_interface('GL-01') hGL2=vessel.get_interface('GL-02') -- Wait until vessels are docked before continuing with script term.out ('Waiting until vessels are docked before') term.out (' executing remainder of script') continue = true hDckPort = hGL1:get_dockhandle(0) while continue do hDckStatus=hGL1:get_dockstatus(hDckPort) if hDckStatus ~= nil then continue = false else proc.wait_simdt(5) end end -- Kill Rotation term.out('Kill Rotation') hGL1:set_navmode(NAVMODE.KILLROT) proc.wait_simdt(10) -- Undock term.out('Undock') hGL1:undock(ALLDOCKS) -- Set RCS mode on GL-01 to Translation term.out('Set RCS mode to translate.') hGL1:set_rcsmode(RCSMODE.LIN) -- Thrust away from GL-02. The resulting distance from GL-02 is about 35 meters. term.out('Separation of GL-01 and GL-02 to +/-35 meters') -- oapi.set_tacc(10) thrstGrpHdl1=hGL1:get_thrustergrouphandle(THGROUP.ATT_BACK) hGL1:set_thrustergrouplevel(THGROUP.ATT_BACK,.1) proc.wait_simdt(11.237) hGL1:set_thrustergrouplevel(THGROUP.ATT_BACK,0) proc.wait_simdt(52.777) thrstGrpHdl2=hGL1:get_thrustergrouphandle(THGROUP.ATT_FORWARD) hGL1:set_thrustergrouplevel(THGROUP.ATT_FORWARD,.1) proc.wait_simdt(18.733) hGL1:set_thrustergrouplevel(THGROUP.ATT_FORWARD,0) -- oapi.set_tacc(1) term.out('Separation completed.') -- Set the prograde autopilot for both vessels to on. term.out('Set prograde autopilot for both vessels.') hGL1:set_navmode(NAVMODE.PROGRADE) hGL2:set_navmode(NAVMODE.PROGRADE) proc.wait_simdt(30) -- The following 14 lines set up the annotations that are used to display -- time to apoapsis for both vessels hApT1Label = oapi.create_annotation() hApT1Label:set_pos(0.7,0.7,1,1) hApT1Label:set_colour({r=1, g=0.7, b=0.3}) hApT1Label:set_text ('ApT (GL-01): ') hApT1 = oapi.create_annotation() hApT1:set_pos(0.8,0.7,1,1) hApT1:set_colour({r=1, g=0.7, b=0.3}) hApT2Label = oapi.create_annotation() hApT2Label:set_pos(0.7,0.75,1,1) hApT2Label:set_colour({r=1, g=0.7, b=0.3}) hApT2Label:set_text ('ApT (GL-02): ') hApT2 = oapi.create_annotation() hApT2:set_pos(0.8,0.75,1,1) hApT2:set_colour({r=1, g=0.7, b=0.3}) -- Wait until +/- 20 seconds before apoapsis, then slow time acceleration to 1x. -- Ignition of main engines on both vessels occurs around +/- 10 seconds before -- apoapsis. Time acceleration during the waiting period is set to 100x to -- reduce waiting time for those who are easily bored. term.out ('Wait until +/- 10 seconds from aoapis. Then fire') term.out (' main engines to stabilize orbit') oapi.set_tacc(100) continue = true while continue do el,op = hGL1:get_elementsex() TimeToApoapsis= op.ApT hApT1:set_text(TimeToApoapsis) el,op=hGL2:get_elementsex() TimeToAposis=op.ApT hApT2:set_text(TimeToApoapsis) if TimeToApoapsis < 20 then continue=false end proc.wait_simdt(1) end oapi.set_tacc(1) -- Track time to apoapsis from time=+/-20 sec in 1x time. continue=true while continue do el,op = hGL1:get_elementsex() TimeToApoapsis1 =op.ApT hApT1:set_text(TimeToApoapsis1) el,op = hGL2:get_elementsex() TimeToApoapsis2=op.ApT hApT2:set_text(TimeToApoapsis2) if TimeToApoapsis1 <= 10 then continue=false oapi.del_annotation(hApT1) oapi.del_annotation(hApT1Label) oapi.del_annotation(hApT2) oapi.del_annotation(hApT2Label) else proc.wait_simdt(1) end end -- Set up annotations to show orbit eccentricities hEcc1Label = oapi.create_annotation() hEcc1Label:set_pos(0.7,0.7,1,1) hEcc1Label:set_colour({r=1, g=0.7, b=0.3}) hEcc1Label:set_text ('Ecc (GL-01): ') hEcc1 = oapi.create_annotation() hEcc1:set_pos(0.8,0.7,1,1) hEcc1:set_colour({r=1, g=0.7, b=0.3}) hEcc2Label = oapi.create_annotation() hEcc2Label:set_pos(0.7,0.75,1,1) hEcc2Label:set_colour({r=1, g=0.7, b=0.3}) hEcc2Label:set_text ('Ecc (GL-02): ') hEcc2 = oapi.create_annotation() hEcc2:set_pos(0.8,0.75,1,1) hEcc2:set_colour({r=1, g=0.7, b=0.3}) -- Stabilize orbits term.out('Start Stabilization of Orbits') hGL1:set_thrustergrouplevel(THGROUP.MAIN, 1) hGL2:set_thrustergrouplevel(THGROUP.MAIN, 1) continue1=true continue2 = true while continue1 or continue2 do el=hGL1:get_elements() e1 = el.e hEcc1:set_text(e1) if e1 <= .005 then hGL1:set_thrustergrouplevel (THGROUP.MAIN, 0) continue1 = false end el = hGL2:get_elements() e2 = el.e hEcc2:set_text(e2) if e2 <= .005 then hGL2:set_thrustergrouplevel (THGROUP.MAIN, 0) continue2 = false end proc.wait_simdt(1) end term.out ('Orbits stabilized.') term.out ('') term.out ('') -- Wait a few seconds and then delete eccentricity annotations proc.wait_simdt(10) oapi.del_annotation(hEcc1) oapi.del_annotation(hEcc1Label) oapi.del_annotation(hEcc2) oapi.del_annotation(hEcc2Label) term.out ('End Script')