238 lines
6.4 KiB
Plaintext
238 lines
6.4 KiB
Plaintext
// functions for calculating steering values.
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// Create a node that will circularize the orbit.
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// 'where' can be one of:
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// the special string "APO", for the next Apoapsis.
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// the special string "PERI", for the next Periapsis.
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// a time value (either a Time struct or a scalar), representing a target time.
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function CreateCircularizationNode {
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parameter where is "APO".
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local t is TIME.
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if where:IsType("String") {
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if where = "APO" {
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set t to TIME + SHIP:ORBIT:ETA:APOAPSIS.
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} else if where = "PERI" {
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set t to TIME + SHIP:ORBIT:ETA:PERIAPSIS.
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} else {
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print "WARNING: Invalid string passed to CreateCirculazationNode(). Node is invalid.".
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}
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} else {
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// we've been passed a time at which to circularize.
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set t to where.
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}
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local Vc is sqrt(SHIP:BODY:MU/(PositionAt(SHIP, t) - SHIP:BODY:POSITION):MAG).
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local dV is Vc - VelocityAt(SHIP, t):ORBIT:MAG.
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local n is Node(t, 0, 0, dV).
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return n.
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}
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// The distance at which to start burning to reach a target on the ground.
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// REQUIRES a circular orbit.
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// TODO: it would be great to semi-automate this...
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function TargetBurnDistance {
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if not HASTARGET {
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return -1.
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}
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return Sqrt(StoppingDistance()^2 + (SHIP:ORBIT:SEMIMAJORAXIS - SHIP:BODY:RADIUS - TARGET:ALTITUDE)^2).
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}
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// Stopping distance at current velocity. For a circular orbit this is valid at any point in the orbit.
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function StoppingDistance {
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local dV is SHIP:VELOCITY:SURFACE:MAG.
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return dV*BurnTime(dV)/2.
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}
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function ExecNode {
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if not HASNODE {
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print "No node to execute.".
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return.
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}
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SAS off.
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// begin the burn at leadT seconds before the node.
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local leadT is BurnTime(NEXTNODE:DELTAV:MAG / 2).
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local t is BurnTime(NEXTNODE:DELTAV:MAG).
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if WillStage(NEXTNODE:DELTAV:MAG) {
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print "WARNING: kOS will stage during this node execution. Safe cancellation requires reboot.".
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when FlameOut() then {
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print "Flameout detected. Staging.".
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stage.
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}
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}
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print "Adjusting heading".
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// The vector constant here should always align our "sides" with the universal up/down axis, so we can predictably place solar panels.
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lock STEERING to LookDirUp(NEXTNODE:DELTAV, V(0,0,90)).
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wait until VAng(SHIP:FACING:FOREVECTOR, STEERINGMANAGER:TARGET:FOREVECTOR) <= 0.1.
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print "Warping to node.".
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KUNIVERSE:TIMEWARP:WarpTo(NEXTNODE:TIME - leadT - 2).
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wait until SHIP:UNPACKED.
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wait until NEXTNODE:ETA <= leadT.
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print "Executing burn.".
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local dvMin is NEXTNODE:DELTAV:MAG.
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lock THROTTLE to 1.0.
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wait t.
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lock THROTTLE to 0.0.
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unlock THROTTLE.
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unlock STEERING.
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SAS on.
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print "Node execution complete.".
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}
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// currently only works for testing against *current* stage.
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function WillStage {
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parameter dV.
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if not HASNODE { return false. }
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return dV > SHIP:StageDeltaV(SHIP:STAGENUM):VACUUM.
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}
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// Calculate the time required to burn a given dV.
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// Assumes a perfectly spherical Kerbal in a vacuum.
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function BurnTime {
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parameter totaldV, s is STAGE:NUMBER.
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local totalT is 0.0.
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local lastStage is false.
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// We allow a small tolerance to deal with potential floating point errors.
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until totaldV <= 0.001 {
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local F is stageThrust(s).
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local Isp is stageISP(s).
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local m is stageMass(s).
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// TODO: handle node execution in atmosphere?
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local dV is min(totaldV, SHIP:StageDeltaV(s):VACUUM).
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local t is calcBurnTime(dV, m, Isp, F).
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set totaldV to totaldV - dV.
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set s to s - 1.
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set totalT to totalT + t.
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}
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return totalT.
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}
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// Convenience function to wrap the actual calculation for burn time.
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function calcBurnTime {
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parameter dV, m, Isp, F.
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if F = 0 or Isp = 0 {
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print "WARNING: Tried to calculate burn time with a denominator value of 0. Returning 0. Your calculations are probably wrong.".
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print "F: " + F .
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print "Isp: " + Isp.
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return 0.
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}
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local g0 is CONSTANT:G0.
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return g0 * m * Isp * (1 - CONSTANT():E^(-dV/(g0*Isp))) / F.
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}
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// Calculate the ISP for a given stage.
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// Defaults to current stage. Assumes your ship is designed so that
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// engines are discarded immediately when they flame out.
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function stageISP {
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parameter s is STAGE:NUMBER.
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local en is list().
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list ENGINES in en.
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local ispSum is 0.
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local eCount is 0.
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for e in en {
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if e:STAGE >= s and e:DECOUPLEDIN < s {
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set ispSum to ispSum + e:VACUUMISP.
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set eCount to eCount + 1.
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}
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}
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if eCount = 0 { return 0. }
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return ispSum / eCount.
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}
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// Calculates the total thrust for the given stage, in kN.
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// Defaults to current stage. Assumes your ship is designed so that
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// engines are discarded immediately when they flame out.
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function stageThrust {
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parameter s is STAGE:NUMBER.
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local en is list().
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list ENGINES in en.
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local sum is 0.
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for e in en {
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if e:STAGE >= s and e:DECOUPLEDIN < s {
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set sum to sum + e:POSSIBLETHRUST.
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}
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}
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return sum.
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}
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// Determine mass at start of target stage.
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// This can handle Delta V-style launchers but
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// only if the central rocket remains in the stack
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// for exactly two stages, one of which is the current stage.
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// More complex staging with partially depleted tanks may produce
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// undefined behavior.
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function stageMass {
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parameter s is STAGE:NUMBER.
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local m is SHIP:MASS.
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if s = SHIP:STAGENUM { return m. }
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local ps is List().
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list PARTS in ps.
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for part in ps {
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if part:DECOUPLEDIN >= s {
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set m to m - part:MASS.
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}
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}
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list ENGINES in ps.
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for part in ps {
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if part:DECOUPLEDIN < s and part:AVAILABLETHRUST > 0 {
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set m to m - (part:MAXMASSFLOW * SHIP:StageDeltaV(SHIP:STAGENUM):DURATION).
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}
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}
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return m.
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}
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// TODO: This would be better in throttle.ks or perhaps some sort of ship status library,
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// but we want to avoid too many inter-dependencies for now.
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function FlameOut {
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local ens is List().
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list engines in ens.
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for en in ens {
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if en:FLAMEOUT {
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return true.
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}
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}
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return false.
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}
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// function PredictGeo {
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// parameter t.
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// local pos is PositionAt(SHIP,t).
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// local rDir is VDOT(SHIP:BODY:NORTH:FOREVECTOR,SHIP:BODY:ANGULARVEL). //the number of radians the body will rotate in one second (negative if rotating counter clockwise when viewed looking down on north
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// local dT is t - TIME:SECONDS.
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// local geoPos is SHIP:BODY:GeoPositionOf(pos).
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// local drift is rDir * dT * CONSTANT:RADTODEG.
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// local long is Mod(geoPos:LNG + drift, 360).
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// if long < -180 {
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// set long to long + 360.
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// }
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// if long > 180 {
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// set long TO long - 360.
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// }
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// return LatLng(geoPos:LAT, long).
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// }
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