void DriveCircularizationBurn(FlightCtrlState s)
{
if (!vessel.patchedConicsUnlocked() || skipCircularization)
{
this.users.Clear();
return;
}
DriveDeployableComponents(s);
if (placedCircularizeNode)
{
if (vessel.patchedConicSolver.maneuverNodes.Count == 0)
{
MechJebModuleFlightRecorder recorder = core.GetComputerModule <MechJebModuleFlightRecorder>();
if (recorder != null)
{
launchPhaseAngle = recorder.phaseAngleFromMark;
}
if (recorder != null)
{
launchLANDifference = vesselState.orbitLAN - recorder.markLAN;
}
//finished circularize
this.users.Clear();
return;
}
}
else
{
//place circularization node
vessel.RemoveAllManeuverNodes();
double UT = orbit.NextApoapsisTime(vesselState.time);
//During the circularization burn, try to correct any inclination errors because it's better to combine the two burns.
// For example, if you're about to do a 1500 m/s circularization burn, if you combine a 200 m/s inclination correction
// into it, you actually only spend 1513 m/s to execute combined manuver. Mechjeb should also do correction burns before
// this if possible, and this can't correct all errors... but it's better then nothing.
// (A better version of this should try to match inclination & LAN if target is specified)
// FIXME? this inclination correction is unlikely to be at tha AN/DN and will throw the LAN off with anything other than high
// TWR launches from equatorial launch sites -- should probably be made optional (or clip it if the correction is too large).
Vector3d inclinationCorrection = OrbitalManeuverCalculator.DeltaVToChangeInclination(orbit, UT, Math.Abs(desiredInclination));
Vector3d smaCorrection = OrbitalManeuverCalculator.DeltaVForSemiMajorAxis(orbit.PerturbedOrbit(UT, inclinationCorrection), UT,
desiredOrbitAltitude + mainBody.Radius);
Vector3d dV = inclinationCorrection + smaCorrection;
vessel.PlaceManeuverNode(orbit, dV, UT);
placedCircularizeNode = true;
core.node.ExecuteOneNode(this);
}
if (core.node.burnTriggered)
{
status = Localizer.Format("#MechJeb_Ascent_status7"); //"Circularizing"
}
else
{
status = Localizer.Format("#MechJeb_Ascent_status8"); //"Coasting to circularization burn"
}
}
private static void DrawnTrajectory(Rect r, MechJebModuleAscentClassic path, MechJebModuleFlightRecorder recorder)
{
if (recorder.history.Length <= 2 || recorder.historyIdx == 0)
{
return;
}
float scale = (float)((path.autoPath ? path.autoTurnEndAltitude : path.turnEndAltitude) / r.height); //meters per pixel
int t = 1;
Vector2 p1 = new Vector2(r.xMin + (float)(recorder.history[0].downRange / scale), r.yMax - (float)(recorder.history[0].altitudeASL / scale));
Vector2 p2 = new Vector2();
while (t <= recorder.historyIdx && t < recorder.history.Length)
{
var rec = recorder.history[t];
p2.x = r.xMin + (float)(rec.downRange / scale);
p2.y = r.yMax - (float)(rec.altitudeASL / scale);
if (r.Contains(p2) && (p1 - p2).sqrMagnitude >= 1.0 || t < 2)
{
Drawing.DrawLine(p1, p2, Color.white, 2, true);
p1.x = p2.x;
p1.y = p2.y;
}
t++;
}
}
public override void OnStart(PartModule.StartState state)
{
width = 128 * hSize;
height = 128 * vSize;
recorder = core.GetComputerModule <MechJebModuleFlightRecorder>();
ResetScale();
}
public override void OnStart(PartModule.StartState state)
{
width = 128 * hSize;
height = 128 * vSize;
recorder = core.GetComputerModule<MechJebModuleFlightRecorder>();
ResetScale();
}
void DriveCircularizationBurn(FlightCtrlState s)
{
if (!vessel.patchedConicsUnlocked() || skipCircularization)
{
this.users.Clear();
return;
}
if (placedCircularizeNode)
{
if (!vessel.patchedConicSolver.maneuverNodes.Any())
{
MechJebModuleFlightRecorder recorder = core.GetComputerModule <MechJebModuleFlightRecorder>();
if (recorder != null)
{
launchPhaseAngle = recorder.phaseAngleFromMark;
}
if (recorder != null)
{
launchLANDifference = vesselState.orbitLAN - recorder.markLAN;
}
//finished circularize
this.users.Clear();
return;
}
}
else
{
//place circularization node
vessel.RemoveAllManeuverNodes();
double UT = orbit.NextApoapsisTime(vesselState.time);
//During the circularization burn, try to correct any inclination errors because it's better to combine the two burns.
// For example, if you're about to do a 1500 m/s circularization burn, if you combine a 200 m/s inclination correction
// into it, you actually only spend 1513 m/s to execute combined manuver. Mechjeb should also do correction burns before
// this if possible, and this can't correct all errors... but it's better then nothing.
// (A better version of this should try to match inclination & LAN if target is specified)
Vector3d inclinationCorrection = OrbitalManeuverCalculator.DeltaVToChangeInclination(orbit, UT, desiredInclination);
Vector3d smaCorrection = OrbitalManeuverCalculator.DeltaVForSemiMajorAxis(orbit.PerturbedOrbit(UT, inclinationCorrection), UT,
desiredOrbitAltitude + mainBody.Radius);
Vector3d dV = inclinationCorrection + smaCorrection;
vessel.PlaceManeuverNode(orbit, dV, UT);
placedCircularizeNode = true;
core.node.ExecuteOneNode(this);
}
if (core.node.burnTriggered)
{
status = "Circularizing";
}
else
{
status = "Coasting to circularization burn";
}
}
public override void OnStart(PartModule.StartState state)
{
if (HighLogic.LoadedSceneIsEditor)
return;
width = 128 * hSize;
height = 128 * vSize;
recorder = core.GetComputerModule<MechJebModuleFlightRecorder>();
ResetScale();
}
public override void OnStart(PartModule.StartState state)
{
if (HighLogic.LoadedSceneIsEditor)
{
return;
}
width = 128 * hSize;
height = 128 * vSize;
recorder = core.GetComputerModule <MechJebModuleFlightRecorder>();
ResetScale();
}
void DriveCircularizationBurn(FlightCtrlState s)
{
if (!vessel.patchedConicsUnlocked() || skipCircularization)
{
this.users.Clear();
return;
}
if (placedCircularizeNode)
{
if (!vessel.patchedConicSolver.maneuverNodes.Any())
{
MechJebModuleFlightRecorder recorder = core.GetComputerModule <MechJebModuleFlightRecorder>();
if (recorder != null)
{
launchPhaseAngle = recorder.phaseAngleFromMark;
}
if (recorder != null)
{
launchLANDifference = vesselState.orbitLAN - recorder.markLAN;
}
//finished circularize
this.users.Clear();
return;
}
}
else
{
//place circularization node
vessel.RemoveAllManeuverNodes();
double UT = orbit.NextApoapsisTime(vesselState.time);
//Vector3d dV = OrbitalManeuverCalculator.DeltaVToCircularize(orbit, UT);
Vector3d dV = OrbitalManeuverCalculator.DeltaVForSemiMajorAxis(orbit, UT, desiredOrbitAltitude + mainBody.Radius);
vessel.PlaceManeuverNode(orbit, dV, UT);
placedCircularizeNode = true;
core.node.ExecuteOneNode(this);
}
if (core.node.burnTriggered)
{
status = "Circularizing";
}
else
{
status = "Coasting to circularization burn";
}
}
public override void OnStart(PartModule.StartState state)
{
path = (DefaultAscentPath)core.GetComputerModule<MechJebModuleAscentAutopilot>().ascentPath;
recorder = core.GetComputerModule<MechJebModuleFlightRecorder>();
}
private static void DrawnTrajectory(Rect r, DefaultAscentPath path, MechJebModuleFlightRecorder recorder)
{
if (recorder.history.Length <= 2 || recorder.historyIdx == 0)
return;
float scale = (float)((path.autoPath ? path.autoTurnEndAltitude : path.turnEndAltitude) / r.height); //meters per pixel
int t = 1;
Vector2 p1 = new Vector2(r.xMin + (float)(recorder.history[0].downRange / scale), r.yMax - (float)(recorder.history[0].altitudeASL / scale));
Vector2 p2 = new Vector2();
while (t <= recorder.historyIdx && t < recorder.history.Length)
{
var rec = recorder.history[t];
p2.x = r.xMin + (float)(rec.downRange / scale);
p2.y = r.yMax - (float)(rec.altitudeASL / scale);
if (r.Contains(p2) && (p1 - p2).sqrMagnitude >= 1.0 || t < 2)
{
Drawing.DrawLine(p1, p2, Color.white, 2, true);
p1.x = p2.x;
p1.y = p2.y;
}
t++;
}
}
public override void OnStart(PartModule.StartState state)
{
autopilot = core.GetComputerModule <MechJebModuleAscentAutopilot>();
recorder = core.GetComputerModule <MechJebModuleFlightRecorder>();
}
public override void OnStart(PartModule.StartState state)
{
path = (DefaultAscentPath)core.GetComputerModule <MechJebModuleAscentAutopilot>().ascentPath;
recorder = core.GetComputerModule <MechJebModuleFlightRecorder>();
}