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finalized raden launch

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wip landing script
This commit is contained in:
Amatsugu
2025-11-20 01:29:40 -05:00
parent 533ec9d520
commit b90b0157e4
8 changed files with 315 additions and 74 deletions
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38
boosterDeorbit.ks Normal file
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//-126
function DeOrbit{
parameter burnLng, deltaV.
lock pos to SHIP:geoposition.
lock curLng to pos:lng.
DECLARE LOCAL tgtLng IS burnLng - 5.
if curLng > burnLng or curLng < tgtLng {
SET WARPMODE TO "RAILS".
SET WARP TO 3.
print "warping to " + tgtLng.
WAIT UNTIL curLng > tgtLng and curLng < burnLng.
SET WARP TO 0.
print "arived at dst " + tgtLng.
print "burn at " + burnLng.
}
print "currently at" + curLng.
BRAKES ON.
RCS ON.
LOCK steering to retrograde.
wait until curLng >= burnLng.
}
function CalculateBurnDuration{
parameter dv.
// declare local isp is GetIsp().
// declare local finalMass is mass * exp(-dv / (isp * constant:g0)).
// declare local twr is ship:maxThrust / (((mass + finalMass)/2) * constant:g0).
// local t is dv / (twr * constant.g0).
// return t.
}

4
boot/radenBoot.ks Normal file
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wait until ship:unpacked.
clearscreen.
switch to 0.
run radenLaunch.

4
boot/sanaBoot.ks Normal file
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wait until ship:unpacked.
clearscreen.
switch to 0.
run poweredLanding.

31
library/lib_math.ks
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@@ -1,15 +1,30 @@
declare function lerp{ declare function Lerp{
parameter a. parameter a.
parameter b. parameter b.
parameter t. parameter t.
return a + (b - a) * t. return a + (b - a) * t.
} }
declare function map{ declare function Map{
parameter a1. parameter value.
parameter b1. parameter low1.
parameter a2. parameter high1.
parameter b2. parameter low2.
parameter v. parameter high2.
return a2 + (v - a1) * (b2 - a2) / (b1 - a1). return low2 + (high2 - low2) * ((value - low1) / (high1 - low1)).
}
declare function ApproximateExp {
parameter x.
local result is 1.0.
local xPower is 1.0.
local nFact is 1.0.
// Loop 4 times (for terms 1 through 4, total 5 terms)
from { local n is 1.} until n = 5 step {set n to n + 1.} do {
SET xPower TO xPower * x.
SET nFact TO nFact * n.
SET result TO result + (xPower / nFact).
}
RETURN result.
} }

112
library/lib_vessel_utils.ks Normal file
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run "library/lib_math".
declare function WaitForEngineStart{
wait until AnyEngineActive().
}
declare function AnyEngineActive{
list engines in allEngines.
for eng in allEngines{
if eng:ignition {
return true.
}
}
return false.
}
declare function GetIsp{
LIST ENGINES IN allEngines.
declare local totalThrust is ship:maxThrust.
local sum is 0.
local weights is 0.
for eng in allEngines{
if eng:IGNITION and not eng:flameout{
local w is eng:AVAILABLETHRUST / totalThrust.
local ispW is eng:isp * w.
set sum to sum + ispW.
set weights to weights + w.
}
}
return sum / weights.
}
declare function GetMaxMassFlow{
LIST ENGINES IN allEngines.
local sum is 0.
for eng in allEngines{
if eng:IGNITION and not eng:flameout{
set sum to sum + eng:maxmassflow.
}
}
return sum.
}
declare function CalculateSuicideBurnAltitude
{
parameter vertSpeed.
parameter localGravity.
parameter tgtAltitude is 0.
local burnAltitude is ((vertSpeed^2) / (2 * CalculateAverageAcceleration(localGravity))).
return burnAltitude + tgtAltitude.
}
declare function CalculateSuicideBurnDuration
{
parameter isp.
return CalculateBurnDuration(verticalSpeed, isp, ship:mass, GetMaxMassFlow() * 1000).
}
declare function CalculateBurnDuration
{
parameter dv.
parameter burnIsp.
parameter initialMass.
parameter massFlow.
set dv to abs(dv).
local exp is -dv / (burnIsp * constant:g0).
local massRatio is ApproximateExp(-exp).
local finalMass is initialMass / massRatio.
local fuelUsed is initialMass - finalMass.
if massFlow <= 0{
return 0.
}
return fuelUsed / massFlow.
}
declare function CalculateAverageAcceleration{
parameter localGravity.
return ((ship:maxthrust * 1000) / ship:mass) - localGravity.
}
declare function GetLocalGravity{
parameter curAltitude is -1.
if curAltitude = -1 {
set curAltitude to altitude.
}
return body:mu / (curAltitude + body:radius)^2.
}
declare function CalculateTimeToImpact{
parameter vertSpeed.
parameter curAltitude.
parameter gravity.
parameter tgtAltitude is 0.
if gravity <= 0 or curAltitude <= 0{
print "[warn]: invalid altitude or gravity.".
return 0.
}
local vs is abs(vertSpeed).
local g is gravity.
local hRel is curAltitude - tgtAltitude.
local disc is ((vs^2) + (2 * g * hRel)).
return (vs + sqrt(disc)) / g.
}

129
poweredLanding.ks
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@@ -1,58 +1,93 @@
run "library/lib_vessel_utils".
run "library/lib_location_constants".
run tests.
//-126 CORE:PART:GETMODULE("kOSProcessor"):DOEVENT("Open Terminal").
function DeOrbit{
parameter burnLng, deltaV.
lock pos to SHIP:geoposition.
lock curLng to pos:lng.
DECLARE LOCAL tgtLng IS burnLng - 5.
if curLng > burnLng or curLng < tgtLng {
SET WARPMODE TO "RAILS".
SET WARP TO 3.
print "warping to " + tgtLng.
WAIT UNTIL curLng > tgtLng and curLng < burnLng.
SET WARP TO 0.
print "arived at dst " + tgtLng.
print "burn at " + burnLng.
}
print "currently at" + curLng.
BRAKES ON.
RCS ON.
LOCK steering to retrograde.
wait until curLng >= burnLng.
function TestSetup{
print "Setting up test".
lock throttle to 100.
wait until apoapsis > 5000.
lock steering to up.
lock throttle to 0.
unlock throttle.
} }
function CalculateBurnDuration{
parameter dv.
declare local isp is GetIsp(). function LandAtPad{
declare local finalMass is mass * exp(-dv / (isp * constant:g0)). print "Starting Landing".
declare local twr is ship:maxThrust / (((mass + finalMass)/2) * constant:g0). gear on.
set pad to location_constants:kerbin:launchpad:position.
lock dist to pad.
lock steering to srfRetrograde.
rcs on.
set landingThrottle to 0.
lock throttle to landingThrottle.
set hoverPid to PIDLoop(5, 0.1, 30, 0, 1).
set tgtAlt to 100.
set hoverPid:setpoint to tgtAlt.
local t is dv / (twr * constant.g0). set landed to false.
return t.
when abs(verticalSpeed) < 10 or verticalSpeed > 1 then{
lock steering to up.
preserve.
} }
function GetIsp{ when verticalSpeed < -10 then{
LIST ENGINES IN allEngines. lock steering to srfRetrograde.
declare local totalThrust is ship:maxThrust. preserve.
local sum is 0.
local weights is 0.
for eng in allEngines{
if eng:IGNITION and not eng:flameout{
local w is eng:AVAILABLETHRUST / totalThrust.
local ispW is eng:isp * w.
set sum to sum + ispW.
set weights to weights + w.
}
}
return sum / weights.
} }
// DeOrbit(-126, 250). until landed {
print CalculateBurnDuration(250). set landingThrottle to hoverPid:update(time:seconds, alt:radar).
// print "offset " + dist.
wait 0.001.
}
}
function Descent{
print "Coasting to apoapsis.".
rcs on.
lock steering to up.
set warp to 1.
wait until verticalSpeed < -100.
set warp to 0.
print "Falling...".
lock steering to srfRetrograde.
brakes on.
local lock vertSpeed to verticalSpeed.
local lock isp to GetIsp().
local lock localGravity to GetLocalGravity(altitude).
local lock burnDuration to CalculateSuicideBurnDuration(isp).
local lock imactTime to CalculateTimeToImpact(abs(vertSpeed), alt:radar, localGravity).
local lock burnAlt to CalculateSuicideBurnAltitude(vertSpeed, localGravity).
local lock timeToBurn to imactTime - burnDuration.
until timeToBurn < 0.5 {
// print "time: " + round(timeToBurn) + " len: " + burnDuration + " impact: " + imactTime + " alt: " + burnAlt.
}
wait until timeToBurn < 0.5.
until abs(verticalSpeed) < 50{
lock throttle to 1.
}
SET V0 TO GETVOICE(0).
V0:PLAY( NOTE(400, 0.5) ).
lock throttle to 0.
}
print "Launch to start.".
WaitForEngineStart().
TestSetup().
Descent().
LandAtPad().

55
radenLaunch.ks
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@@ -1,28 +1,47 @@
run "library/lib_math". run "library/lib_math".
run "library/lib_vessel_utils".
local athmoAccelTarget is 600.
CORE:PART:GETMODULE("kOSProcessor"):DOEVENT("Open Terminal").
clearScreen. clearScreen.
BRAKES on. BRAKES on.
print "Waiting for engine ignition".
WaitForEngineStart().
print "Preparing to launch". print "Preparing to launch".
from { local c is 5.} until c = 0 step {set c to c - 1.} do { from { local c is 5.} until c = 0 step {set c to c - 1.} do {
print c. print c.
wait 1. wait 1.
} }
clearScreen.
print "Launching!". print "Launching!".
lock throttle to 100. // stage.
lock steering to heading(90, 0, 0). lock throttle to 1.
lock steering to heading(90, 1).
brakes off.
sas off.
print "Phase: Takeoff". print "Phase: Takeoff".
wait until surfaceSpeed > 140.
wait until groundspeed > 120.
print "Phase: Rotate". print "Phase: Rotate".
lock steering to heading(90, 3, 0). lock steering to heading(90, 4).
wait 1. wait until altitude > 80.
print "Gear up". print "Gear up".
gear off. gear off.
print "Phase: Athmospheric Acceleration".
lock steering to heading(90, 3, 0).
wait until groundspeed > athmoAccelTarget.
print "Phase: Athmospheric Climb". print "Phase: Athmospheric Climb".
lock steering to heading(90, 15, 0). lock tgtPitch to Map(groundSpeed, athmoAccelTarget, 1600, 3, 15).
wait until altitude > 20000. lock steering to heading(90, tgtPitch, 0).
wait until altitude > 25000.
print "Phase: Mode Switch". print "Phase: Mode Switch".
ag1 on. //Switch engine mode ag1 on. //Switch engine mode
@@ -31,20 +50,28 @@ wait until apoapsis > 80000.
print "Phase: Sub-Orbital Coast". print "Phase: Sub-Orbital Coast".
lock throttle to 0. lock throttle to 0.
lock steering to prograde. set warpmode to "physics".
set warp to 1.
when altitude > 70000 then { wait until altitude > 70000.
print "Deploying Solar". print "Deploying Solar".
ag2 on. //deploy solar panels on. //deploy solar
print "Opening Docking Port". print "Opening Docking Port".
ag3 on. //open docking port ag3 on. //open docking port
} lock steering to heading(90, 0, 0).
set warp to 0.
set warpmode to "rails".
set warp to 1.
lock distToApo to apoapsis - altitude. lock distToApo to apoapsis - altitude.
wait until distToApo < 100. wait until distToApo < 500.
print "Phase: Circularize". print "Phase: Circularize".
lock throttle to 100. lock steering to heading(90, 0, 0).
wait until periapsis > 79000. rcs on.
lock throttle to 1.
wait until periapsis > 75000.
unlock throttle. unlock throttle.
print "In orbit. Releasing controls". print "In orbit. Releasing controls".

6
tests.ks Normal file
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run "library/lib_vessel_utils".
CORE:PART:GETMODULE("kOSProcessor"):DOEVENT("Open Terminal").
print "impact " + CalculateTimeToImpact(300, 500, 9.8).
print "Burn Duration" + CalculateBurnDuration(300, 350, 5000, 3000).