Difference between revisions of "Lua Script for Orbit Stabilization"
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Line 45: | Line 45: | ||
while continue do | while continue do | ||
− | hDckStatus=hGL1:get_dockstatus(hDckPort) | + | hDckStatus=hGL1:get_dockstatus(hDckPort) |
if hDckStatus ~= nil then | if hDckStatus ~= nil then |
Revision as of 19:42, 12 July 2019
-- 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)
continue=true
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(25)
-- 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')