public void RCSBalancerInfoItem()
{
GUILayout.BeginVertical();
GuiUtils.SimpleLabel("Calculation time", (solverThread.calculationTime * 1000).ToString("F0") + " ms");
GuiUtils.SimpleLabelInt("Pending tasks", solverThread.taskCount);
GuiUtils.SimpleLabelInt("Cache size", solverThread.cacheSize);
GuiUtils.SimpleLabelInt("Cache hits", solverThread.cacheHits);
GuiUtils.SimpleLabelInt("Cache misses", solverThread.cacheMisses);
GuiUtils.SimpleLabel("CoM shift", MuUtils.ToSI(solverThread.comError) + "m");
GuiUtils.SimpleLabel("CoM recalc", MuUtils.ToSI(solverThread.comErrorThreshold) + "m");
GuiUtils.SimpleLabel("Max CoM shift", MuUtils.ToSI(solverThread.maxComError) + "m");
GuiUtils.SimpleLabel("Status", solverThread.statusString);
string error = solverThread.errorString;
if (!string.IsNullOrEmpty(error))
{
GUILayout.Label(error, GUILayout.ExpandWidth(true));
}
GUILayout.EndVertical();
}
public string TargetSMA()
{
if (!core.target.NormalTargetExists)
{
return("N/A");
}
return(MuUtils.ToSI(core.target.TargetOrbit.semiMajorAxis, 2) + "m");
}
public string TargetOrbitSpeed()
{
if (!core.target.NormalTargetExists)
{
return("N/A");
}
return(MuUtils.ToSI(core.target.TargetOrbit.GetVel().magnitude) + "m/s");
}
public string TargetPeriapsis()
{
if (!core.target.NormalTargetExists)
{
return("N/A");
}
return(MuUtils.ToSI(core.target.TargetOrbit.PeA, 2) + "m");
}
public string TargetRelativeVelocity()
{
if (!core.target.NormalTargetExists)
{
return("N/A");
}
return(MuUtils.ToSI(core.target.RelativeVelocity.magnitude) + "m/s");
}
public string TargetDistance()
{
if (core.target.Target == null)
{
return("N/A");
}
return(MuUtils.ToSI(core.target.Distance, -1) + "m");
}
public string TargetApoapsis()
{
if (!core.target.NormalTargetExists)
{
return("N/A");
}
return(MuUtils.ToSI(core.target.Orbit.ApA, 2) + "m");
}
protected override void WindowGUI(int windowID)
{
GUILayout.BeginVertical();
GUIStyle s = new GUIStyle(GUI.skin.label);
s.alignment = TextAnchor.MiddleCenter;
List <Runway> availableRunways = MechJebModuleSpaceplaneAutopilot.runways.Where(p => p.body == mainBody).ToList();
if (runwayIndex > availableRunways.Count)
{
runwayIndex = 0;
}
if (availableRunways.Any())
{
GUILayout.Label(Localizer.Format("#MechJeb_ApproAndLand_label1"), s);//Landing
runwayIndex = GuiUtils.ComboBox.Box(runwayIndex, availableRunways.Select(p => p.name).ToArray(), this);
autoland.runway = availableRunways[runwayIndex];
GUILayout.Label(Localizer.Format("#MechJeb_ApproAndLand_label2") + MuUtils.ToSI(Vector3d.Distance(vesselState.CoM, autoland.runway.Start()), 0) + "m"); //Distance to runway:
showLandingTarget = GUILayout.Toggle(showLandingTarget, Localizer.Format("#MechJeb_ApproAndLand_label3")); //Show landing navball guidance
if (GUILayout.Button(Localizer.Format("#MechJeb_ApproAndLan_button1"))) //Autoland
{
autoland.Autoland(this);
}
if (autoland.enabled && GUILayout.Button(Localizer.Format("#MechJeb_ApproAndLan_button2")))//Abort
{
autoland.AutopilotOff();
}
GuiUtils.SimpleTextBox(Localizer.Format("#MechJeb_ApproAndLand_label14"), autoland.glideslope, "°"); //Autoland glideslope:
GuiUtils.SimpleTextBox(Localizer.Format("#MechJeb_ApproAndLand_label4"), autoland.approachSpeed, "m/s"); //Approach speed:
GuiUtils.SimpleTextBox(Localizer.Format("#MechJeb_ApproAndLand_label5"), autoland.touchdownSpeed, "m/s"); //Touchdown speed:
autoland.bEngageReverseIfAvailable = GUILayout.Toggle(autoland.bEngageReverseIfAvailable, Localizer.Format("#MechJeb_ApproAndLand_label6")); //Reverse thrust upon touchdown
autoland.bBreakAsSoonAsLanded = GUILayout.Toggle(autoland.bBreakAsSoonAsLanded, Localizer.Format("#MechJeb_ApproAndLand_label7")); //Brake as soon as landed
if (autoland.enabled)
{
GUILayout.Label(Localizer.Format("#MechJeb_ApproAndLand_label8") + autoland.AutolandApproachStateToHumanReadableDescription()); //State:
GUILayout.Label(Localizer.Format("#MechJeb_ApproAndLand_label9", Math.Round(autoland.GetAutolandLateralDistanceToNextWaypoint(), 0))); //Distance to waypoint: {0}m
//GUILayout.Label(string.Format("Distance to waypoint: {0} m", Math.Round(autoland.GetAutolandLateralDistanceToNextWaypoint(), 0)));
GUILayout.Label(Localizer.Format("#MechJeb_ApproAndLand_label10", Math.Round(autoland.Autopilot.SpeedTarget, 1))); //Target speed: {0} m/s
GUILayout.Label(Localizer.Format("#MechJeb_ApproAndLand_label11", Math.Round(autoland.GetAutolandTargetAltitude(autoland.GetAutolandTargetVector()), 0))); //Target altitude: {0} m
GUILayout.Label(Localizer.Format("#MechJeb_ApproAndLand_label12", Math.Round(autoland.Autopilot.VertSpeedTarget, 1))); //Target vertical speed: {0} m/s
GUILayout.Label(Localizer.Format("#MechJeb_ApproAndLand_label13", Math.Round(autoland.Autopilot.HeadingTarget, 0))); //Target heading: {0}º
}
}
GUILayout.EndVertical();
base.WindowGUI(windowID);
}
public string NextManeuverNodeDeltaV()
{
if (!vessel.patchedConicsUnlocked() || !vessel.patchedConicSolver.maneuverNodes.Any())
{
return("N/A");
}
return(MuUtils.ToSI(vessel.patchedConicSolver.maneuverNodes[0].GetBurnVector(orbit).magnitude, -1) + "m/s");
}
protected override void WindowGUI(int windowID)
{
GUILayout.BeginVertical();
GUIStyle s = new GUIStyle(GUI.skin.label);
s.alignment = TextAnchor.MiddleCenter;
List <Runway> availableRunways = MechJebModuleSpaceplaneAutopilot.runways.Where(p => p.body == mainBody).ToList();
if (runwayIndex > availableRunways.Count)
{
runwayIndex = 0;
}
if (availableRunways.Any())
{
GUILayout.Label("Landing", s);
runwayIndex = GuiUtils.ComboBox.Box(runwayIndex, availableRunways.Select(p => p.name).ToArray(), this);
autoland.runway = availableRunways[runwayIndex];
GUILayout.Label("Distance to runway: " + MuUtils.ToSI(Vector3d.Distance(vesselState.CoM, autoland.runway.Start()), 0) + "m");
showLandingTarget = GUILayout.Toggle(showLandingTarget, "Show landing navball guidance");
if (GUILayout.Button("Autoland"))
{
autoland.Autoland(this);
}
if (autoland.enabled && GUILayout.Button("Abort"))
{
autoland.AutopilotOff();
}
GuiUtils.SimpleTextBox("Autoland glideslope:", autoland.glideslope);
GuiUtils.SimpleTextBox("Approach speed:", autoland.approachSpeed);
GuiUtils.SimpleTextBox("Touchdown speed:", autoland.touchdownSpeed);
autoland.bEngageReverseIfAvailable = GUILayout.Toggle(autoland.bEngageReverseIfAvailable, "Reverse thrust upon touchdown");
autoland.bBreakAsSoonAsLanded = GUILayout.Toggle(autoland.bBreakAsSoonAsLanded, "Break As Soon As Landed");
if (autoland.enabled)
{
GUILayout.Label("State: " + autoland.AutolandApproachStateToHumanReadableDescription());
GUILayout.Label(string.Format("Distance to waypoint: {0} m", Math.Round(autoland.GetAutolandLateralDistanceToNextWaypoint(), 0)));
GUILayout.Label(string.Format("Target speed: {0} m/s", Math.Round(autoland.Autopilot.SpeedTarget, 1)));
GUILayout.Label(string.Format("Target altitude: {0} m", Math.Round(autoland.GetAutolandTargetAltitude(autoland.GetAutolandTargetVector()), 0)));
GUILayout.Label(string.Format("Target vertical speed: {0} m/s", Math.Round(autoland.Autopilot.VertSpeedTarget, 1)));
GUILayout.Label(string.Format("Target heading: {0}º", Math.Round(autoland.Autopilot.HeadingTarget, 0)));
}
}
GUILayout.EndVertical();
base.WindowGUI(windowID);
}
protected override void WindowGUI(int windowID)
{
GUILayout.BeginVertical();
GUIStyle s = new GUIStyle(GUI.skin.label);
s.alignment = TextAnchor.MiddleCenter;
GUILayout.Label("Landing", s);
Runway[] runways = MechJebModuleSpaceplaneAutopilot.runways;
int runwayIndex = Array.IndexOf(runways, autopilot.runway);
runwayIndex = GuiUtils.ArrowSelector(runwayIndex, runways.Length, autopilot.runway.name);
autopilot.runway = runways[runwayIndex];
GUILayout.Label("Distance to runway: " + MuUtils.ToSI(Vector3d.Distance(vesselState.CoM, autopilot.runway.Start(vesselState.CoM)), 0) + "m");
showLandingTarget = GUILayout.Toggle(showLandingTarget, "Show landing navball guidance");
if (GUILayout.Button("Autoland"))
{
autopilot.Autoland(this);
}
if (autopilot.enabled && autopilot.mode == MechJebModuleSpaceplaneAutopilot.Mode.AUTOLAND &&
GUILayout.Button("Abort"))
{
autopilot.AutopilotOff();
}
GuiUtils.SimpleTextBox("Autoland glideslope:", autopilot.glideslope, "º");
GUILayout.Label("Hold", s);
GUILayout.BeginHorizontal();
if (GUILayout.Button("Initiate hold:"))
{
autopilot.HoldHeadingAndAltitude(this);
}
GUILayout.Label("Heading:");
autopilot.targetHeading.text = GUILayout.TextField(autopilot.targetHeading.text, GUILayout.Width(40));
GUILayout.Label("º Altitude:");
autopilot.targetAltitude.text = GUILayout.TextField(autopilot.targetAltitude.text, GUILayout.Width(40));
GUILayout.Label("m");
GUILayout.EndHorizontal();
if (autopilot.enabled && autopilot.mode == MechJebModuleSpaceplaneAutopilot.Mode.HOLD &&
GUILayout.Button("Abort"))
{
autopilot.AutopilotOff();
}
GUILayout.EndVertical();
base.WindowGUI(windowID);
}
public string OrbitSummary(Orbit o)
{
if (o.eccentricity > 1)
{
return("hyperbolic, Pe = " + MuUtils.ToSI(o.PeA, 2) + "m");
}
else
{
return(MuUtils.ToSI(o.PeA, 2) + "m x " + MuUtils.ToSI(o.ApA, 2) + "m");
}
}
public string TargetClosestApproachDistance()
{
if (!core.target.NormalTargetExists)
{
return("N/A");
}
if (core.target.Orbit.referenceBody != orbit.referenceBody)
{
return("N/A");
}
return(MuUtils.ToSI(orbit.NextClosestApproachDistance(core.target.Orbit, vesselState.time), -1) + "m");
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
if (o.referenceBody.Radius + newApA < o.Radius(UT))
{
string burnAltitude = MuUtils.ToSI(o.Radius(UT) - o.referenceBody.Radius) + "m";
throw new OperationException(Localizer.Format("#MechJeb_Ap_Exception", burnAltitude));//new apoapsis cannot be lower than the altitude of the burn (<<1>>)
}
return(new ManeuverParameters(OrbitalManeuverCalculator.DeltaVToChangeApoapsis(o, UT, newApA + o.referenceBody.Radius), UT));
}
public string TargetClosestApproachRelativeVelocity()
{
if (!core.target.NormalTargetExists)
{
return("N/A");
}
if (core.target.Orbit.referenceBody != orbit.referenceBody)
{
return("N/A");
}
double UT = orbit.NextClosestApproachTime(core.target.Orbit, vesselState.time);
double relVel = (orbit.SwappedOrbitalVelocityAtUT(UT) - core.target.Orbit.SwappedOrbitalVelocityAtUT(UT)).magnitude;
return(MuUtils.ToSI(relVel, -1) + "m/s");
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
if (o.referenceBody.Radius + newPeA > o.Radius(UT))
{
string burnAltitude = MuUtils.ToSI(o.Radius(UT) - o.referenceBody.Radius) + "m";
throw new Exception("new periapsis cannot be higher than the altitude of the burn (" + burnAltitude + ")");
}
else if (newPeA < -o.referenceBody.Radius)
{
throw new Exception("new periapsis cannot be lower than minus the radius of " + o.referenceBody.theName + "(-" + MuUtils.ToSI(o.referenceBody.Radius, 3) + "m)");
}
return(new ManeuverParameters(OrbitalManeuverCalculator.DeltaVToChangePeriapsis(o, UT, newPeA + o.referenceBody.Radius), UT));
}
void DrawGUIPrediction()
{
ReentrySimulation.Result result = predictor.Result;
if (result != null)
{
switch (result.outcome)
{
case ReentrySimulation.Outcome.LANDED:
GUILayout.Label("Landing Predictions:");
GUILayout.Label(Coordinates.ToStringDMS(result.endPosition.latitude, result.endPosition.longitude) + "\nASL:" + MuUtils.ToSI(result.endASL, -1, 4) + "m");
GUILayout.Label(result.body.GetExperimentBiomeSafe(result.endPosition.latitude, result.endPosition.longitude));
double error = Vector3d.Distance(mainBody.GetWorldSurfacePosition(result.endPosition.latitude, result.endPosition.longitude, 0) - mainBody.position,
mainBody.GetWorldSurfacePosition(core.target.targetLatitude, core.target.targetLongitude, 0) - mainBody.position);
GUILayout.Label("Target difference = " + MuUtils.ToSI(error, 0) + "m"
+ "\nMax drag: " + result.maxDragGees.ToString("F1") + "g"
+ "\nDelta-v needed: " + result.deltaVExpended.ToString("F1") + "m/s"
+ "\nTime to land: " + (vessel.Landed ? "0.0s" : GuiUtils.TimeToDHMS(result.endUT - Planetarium.GetUniversalTime(), 1)));
break;
case ReentrySimulation.Outcome.AEROBRAKED:
GUILayout.Label("Predicted orbit after aerobraking:");
Orbit o = result.AeroBrakeOrbit();
if (o.eccentricity > 1)
{
GUILayout.Label("Hyperbolic, eccentricity = " + o.eccentricity.ToString("F2"));
}
else
{
GUILayout.Label(MuUtils.ToSI(o.PeA, 3) + "m x " + MuUtils.ToSI(o.ApA, 3) + "m");
}
GUILayout.Label("Max drag: " + result.maxDragGees.ToString("F1") + "g"
+ "\nExit atmosphere in: " + GuiUtils.TimeToDHMS(result.aeroBrakeUT - Planetarium.GetUniversalTime(), 1));
break;
case ReentrySimulation.Outcome.NO_REENTRY:
GUILayout.Label("Orbit does not reenter:\n"
+ MuUtils.ToSI(orbit.PeA, 3) + "m Pe > " + MuUtils.ToSI(mainBody.RealMaxAtmosphereAltitude(), 3) + (mainBody.atmosphere ? "m atmosphere height" : "m ground"));
break;
case ReentrySimulation.Outcome.TIMED_OUT:
GUILayout.Label("Reentry simulation timed out.");
break;
}
}
}
void DrawGUIPrediction()
{
ReentrySimulation.Result result = predictor.GetResult();
if (result != null)
{
switch (result.outcome)
{
case ReentrySimulation.Outcome.LANDED:
GUILayout.Label("Predicted landing site:");
GUILayout.Label(Coordinates.ToStringDMS(result.endPosition.latitude, result.endPosition.longitude));
double error = Vector3d.Distance(mainBody.GetRelSurfacePosition(result.endPosition.latitude, result.endPosition.longitude, 0),
mainBody.GetRelSurfacePosition(core.target.targetLatitude, core.target.targetLongitude, 0));
GUILayout.Label("Difference from target = " + MuUtils.ToSI(error, 0) + "m");
if (result.maxDragGees > 0)
{
GUILayout.Label("Predicted max drag gees: " + result.maxDragGees.ToString("F1"));
}
break;
case ReentrySimulation.Outcome.AEROBRAKED:
GUILayout.Label("Predicted orbit after aerobraking:");
Orbit o = result.EndOrbit();
if (o.eccentricity > 1)
{
GUILayout.Label("Hyperbolic, eccentricity = " + o.eccentricity.ToString("F2"));
}
else
{
GUILayout.Label(MuUtils.ToSI(o.PeA, 3) + "m x " + MuUtils.ToSI(o.ApA, 3) + "m");
}
break;
case ReentrySimulation.Outcome.NO_REENTRY:
GUILayout.Label("Orbit does not reenter:");
GUILayout.Label(MuUtils.ToSI(orbit.PeA, 3) + "m Pe > " + MuUtils.ToSI(mainBody.RealMaxAtmosphereAltitude(), 3) + "m atmosphere height");
break;
case ReentrySimulation.Outcome.TIMED_OUT:
GUILayout.Label("Reentry simulation timed out.");
break;
}
}
}
public override List <ManeuverParameters> MakeNodesImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
if (o.referenceBody.Radius + newPeA > o.Radius(UT))
{
string burnAltitude = MuUtils.ToSI(o.Radius(UT) - o.referenceBody.Radius) + "m";
throw new OperationException(Localizer.Format("#MechJeb_Pe_Exception1") + " (" + burnAltitude + ")");//new periapsis cannot be higher than the altitude of the burn
}
else if (newPeA < -o.referenceBody.Radius)
{
throw new OperationException(Localizer.Format("#MechJeb_Pe_Exception2", o.referenceBody.displayName) + "(-" + MuUtils.ToSI(o.referenceBody.Radius, 3) + "m)");//new periapsis cannot be lower than minus the radius of <<1>>
}
List <ManeuverParameters> NodeList = new List <ManeuverParameters>();
NodeList.Add(new ManeuverParameters(OrbitalManeuverCalculator.DeltaVToChangePeriapsis(o, UT, newPeA + o.referenceBody.Radius), UT));
return(NodeList);
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
string burnAltitude = MuUtils.ToSI(o.Radius(UT) - o.referenceBody.Radius) + "m";
if (o.referenceBody.Radius + newPeA > o.Radius(UT))
{
throw new OperationException(Localizer.Format("#MechJeb_both_Exception1", burnAltitude));//new periapsis cannot be higher than the altitude of the burn (<<1>>)
}
else if (o.referenceBody.Radius + newApA < o.Radius(UT))
{
throw new OperationException(Localizer.Format("#MechJeb_both_Exception2") + "(" + burnAltitude + ")");//new apoapsis cannot be lower than the altitude of the burn
}
else if (newPeA < -o.referenceBody.Radius)
{
throw new OperationException(Localizer.Format("#MechJeb_both_Exception3") + o.referenceBody.displayName + "(-" + MuUtils.ToSI(o.referenceBody.Radius, 3) + "m)");//"new periapsis cannot be lower than minus the radius of "
}
return(new ManeuverParameters(OrbitalManeuverCalculator.DeltaVToEllipticize(o, UT, newPeA + o.referenceBody.Radius, newApA + o.referenceBody.Radius), UT));
}
protected override void WindowGUI(int windowID)
{
if (!core.target.NormalTargetExists)
{
GUILayout.Label("Select a target to rendezvous with.");
base.WindowGUI(windowID);
return;
}
if (core.target.Orbit.referenceBody != orbit.referenceBody)
{
GUILayout.Label("Rendezvous target must be in the same sphere of influence.");
base.WindowGUI(windowID);
return;
}
GUILayout.BeginVertical();
//Information readouts:
GuiUtils.SimpleLabel("Rendezvous target", core.target.Name);
double leadTime = 30;
GuiUtils.SimpleLabel("Target orbit", MuUtils.ToSI(core.target.Orbit.PeA, 3) + "m x " + MuUtils.ToSI(core.target.Orbit.ApA, 3) + "m");
GuiUtils.SimpleLabel("Current orbit", MuUtils.ToSI(orbit.PeA, 3) + "m x " + MuUtils.ToSI(orbit.ApA, 3) + "m");
GuiUtils.SimpleLabel("Relative inclination", orbit.RelativeInclination(core.target.Orbit).ToString("F2") + "º");
double closestApproachTime = orbit.NextClosestApproachTime(core.target.Orbit, vesselState.time);
GuiUtils.SimpleLabel("Time until closest approach", GuiUtils.TimeToDHMS(closestApproachTime - vesselState.time));
GuiUtils.SimpleLabel("Separation at closest approach", MuUtils.ToSI(orbit.Separation(core.target.Orbit, closestApproachTime), 0) + "m");
//Maneuver planning buttons:
if (GUILayout.Button("Align Planes"))
{
double UT;
Vector3d dV;
if (orbit.AscendingNodeExists(core.target.Orbit))
{
dV = OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesAscending(orbit, core.target.Orbit, vesselState.time, out UT);
}
else
{
dV = OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesDescending(orbit, core.target.Orbit, vesselState.time, out UT);
}
vessel.RemoveAllManeuverNodes();
vessel.PlaceManeuverNode(orbit, dV, UT);
}
GUILayout.BeginHorizontal();
if (GUILayout.Button("Establish new orbit at"))
{
double phasingOrbitRadius = phasingOrbitAltitude + mainBody.Radius;
vessel.RemoveAllManeuverNodes();
if (orbit.ApR < phasingOrbitRadius)
{
double UT1 = vesselState.time + leadTime;
Vector3d dV1 = OrbitalManeuverCalculator.DeltaVToChangeApoapsis(orbit, UT1, phasingOrbitRadius);
vessel.PlaceManeuverNode(orbit, dV1, UT1);
Orbit transferOrbit = vessel.patchedConicSolver.maneuverNodes[0].nextPatch;
double UT2 = transferOrbit.NextApoapsisTime(UT1);
Vector3d dV2 = OrbitalManeuverCalculator.DeltaVToCircularize(transferOrbit, UT2);
vessel.PlaceManeuverNode(transferOrbit, dV2, UT2);
}
else if (orbit.PeR > phasingOrbitRadius)
{
double UT1 = vesselState.time + leadTime;
Vector3d dV1 = OrbitalManeuverCalculator.DeltaVToChangePeriapsis(orbit, UT1, phasingOrbitRadius);
vessel.PlaceManeuverNode(orbit, dV1, UT1);
Orbit transferOrbit = vessel.patchedConicSolver.maneuverNodes[0].nextPatch;
double UT2 = transferOrbit.NextPeriapsisTime(UT1);
Vector3d dV2 = OrbitalManeuverCalculator.DeltaVToCircularize(transferOrbit, UT2);
vessel.PlaceManeuverNode(transferOrbit, dV2, UT2);
}
else
{
double UT = orbit.NextTimeOfRadius(vesselState.time, phasingOrbitRadius);
Vector3d dV = OrbitalManeuverCalculator.DeltaVToCircularize(orbit, UT);
vessel.PlaceManeuverNode(orbit, dV, UT);
}
}
phasingOrbitAltitude.text = GUILayout.TextField(phasingOrbitAltitude.text, GUILayout.Width(70));
GUILayout.Label("km", GUILayout.ExpandWidth(false));
GUILayout.EndHorizontal();
if (GUILayout.Button("Intercept with Hohmann transfer"))
{
double UT;
Vector3d dV = OrbitalManeuverCalculator.DeltaVAndTimeForHohmannTransfer(orbit, core.target.Orbit, vesselState.time, out UT);
vessel.RemoveAllManeuverNodes();
vessel.PlaceManeuverNode(orbit, dV, UT);
}
if (GUILayout.Button("Match velocities at closest approach"))
{
double UT = closestApproachTime;
Vector3d dV = OrbitalManeuverCalculator.DeltaVToMatchVelocities(orbit, UT, core.target.Orbit);
vessel.RemoveAllManeuverNodes();
vessel.PlaceManeuverNode(orbit, dV, UT);
}
if (GUILayout.Button("Get closer"))
{
double UT = vesselState.time;
double interceptUT = UT + 100;
Vector3d dV = OrbitalManeuverCalculator.DeltaVToInterceptAtTime(orbit, UT, core.target.Orbit, interceptUT, 10);
vessel.RemoveAllManeuverNodes();
vessel.PlaceManeuverNode(orbit, dV, UT);
}
GUILayout.EndVertical();
base.WindowGUI(windowID);
}
string GetStringValue(object value)
{
if (value == null)
{
return("null");
}
if (value is string)
{
return((string)value + " " + units);
}
if (value is int)
{
return(((int)value).ToString() + " " + units);
}
double doubleValue = -999;
if (value is double)
{
doubleValue = (double)value;
}
else if (value is float)
{
doubleValue = (float)value;
}
else if (value is MovingAverage)
{
doubleValue = (MovingAverage)value;
}
else if (value is Vector3d)
{
doubleValue = ((Vector3d)value).magnitude;
}
else if (value is Vector3)
{
doubleValue = ((Vector3)value).magnitude;
}
else if (value is EditableDouble)
{
doubleValue = (EditableDouble)value;
}
if (format == TIME)
{
return(GuiUtils.TimeToDHMS(doubleValue, timeDecimalPlaces));
}
else if (format == ANGLE)
{
return(Coordinates.AngleToDMS(doubleValue));
}
else if (format == ANGLE_NS)
{
return(Coordinates.AngleToDMS(doubleValue) + " " + (doubleValue > 0 ? "N" : "S"));
}
else if (format == ANGLE_EW)
{
return(Coordinates.AngleToDMS(doubleValue) + " " + (doubleValue > 0 ? "E" : "W"));
}
else if (format == SI)
{
return(MuUtils.ToSI(doubleValue, siMaxPrecision, siSigFigs) + units);
}
else
{
return(doubleValue.ToString(format) + " " + units);
}
}
protected override void WindowGUI(int windowID)
{
if (path == null)
{
GUILayout.Label("Path is null!!!1!!1!1!1111!11eleven");
base.WindowGUI(windowID);
}
GUILayout.BeginVertical();
double oldTurnStartAltitude = path.turnStartAltitude;
double oldTurnEndAltitude = path.turnEndAltitude;
double oldTurnShapeExponent = path.turnShapeExponent;
double oldTurnEndAngle = path.turnEndAngle;
GUILayout.BeginHorizontal();
path.autoPath = GUILayout.Toggle(path.autoPath, "Automatic Altitude Turn", GUILayout.ExpandWidth(false));
if (path.autoPath)
{
path.autoTurnPerc = Mathf.Floor(GUILayout.HorizontalSlider(path.autoTurnPerc, 0.01f, 1.05f) * 200f + 0.5f) / 200f;
}
GUILayout.EndHorizontal();
if (path.autoPath)
{
GUILayout.BeginHorizontal();
GUILayout.Label("Turn start altitude: ");
GUILayout.Label(MuUtils.ToSI(path.autoTurnStartAltitude, -1, 2) + "m", new GUIStyle(GUI.skin.label)
{
alignment = TextAnchor.MiddleRight
}, GUILayout.ExpandWidth(true));
GUILayout.EndHorizontal();
GUILayout.BeginHorizontal();
GUILayout.Label("Turn end altitude: ");
GUILayout.Label(MuUtils.ToSI(path.autoTurnEndAltitude, -1, 2) + "m", new GUIStyle(GUI.skin.label)
{
alignment = TextAnchor.MiddleRight
}, GUILayout.ExpandWidth(true));
GUILayout.EndHorizontal();
}
else
{
GuiUtils.SimpleTextBox("Turn start altitude:", path.turnStartAltitude, "km");
GuiUtils.SimpleTextBox("Turn end altitude:", path.turnEndAltitude, "km");
}
GuiUtils.SimpleTextBox("Final flight path angle:", path.turnEndAngle, "°");
GuiUtils.SimpleTextBox("Turn shape:", path.turnShapeExponent, "%");
// Round the slider's value (0..1) to sliderPrecision decimal places.
int sliderPrecision = 3;
double sliderTurnShapeExponent = GUILayout.HorizontalSlider((float)path.turnShapeExponent, 0.0F, 1.0F);
if (Math.Round(Math.Abs(sliderTurnShapeExponent - oldTurnShapeExponent), sliderPrecision) > 0)
{
path.turnShapeExponent = new EditableDoubleMult(Math.Round(sliderTurnShapeExponent, sliderPrecision), 0.01);
}
GUILayout.Box(pathTexture);
GUILayout.EndVertical();
if (path.turnStartAltitude != oldTurnStartAltitude ||
path.turnEndAltitude != oldTurnEndAltitude ||
path.turnShapeExponent != oldTurnShapeExponent ||
path.turnEndAngle != oldTurnEndAngle ||
!pathTextureDrawnBefore)
{
UpdatePathTexture();
}
base.WindowGUI(windowID);
}
protected override void WindowGUI(int windowID)
{
GUILayout.BeginVertical();
if (core.target.PositionTargetExists)
{
var ASL = core.vessel.mainBody.TerrainAltitude(core.target.targetLatitude, core.target.targetLongitude);
GUILayout.Label("Target coordinates:");
GUILayout.BeginHorizontal();
core.target.targetLatitude.DrawEditGUI(EditableAngle.Direction.NS);
if (GUILayout.Button("▲"))
{
moveByMeter(ref core.target.targetLatitude, 10, ASL);
}
GUILayout.Label("10m");
if (GUILayout.Button("▼"))
{
moveByMeter(ref core.target.targetLatitude, -10, ASL);
}
GUILayout.EndHorizontal();
GUILayout.BeginHorizontal();
core.target.targetLongitude.DrawEditGUI(EditableAngle.Direction.EW);
if (GUILayout.Button("◄"))
{
moveByMeter(ref core.target.targetLongitude, -10, ASL);
}
GUILayout.Label("10m");
if (GUILayout.Button("►"))
{
moveByMeter(ref core.target.targetLongitude, 10, ASL);
}
GUILayout.EndHorizontal();
GUILayout.BeginHorizontal();
GUILayout.Label("ASL: " + MuUtils.ToSI(ASL, -1, 4) + "m");
GUILayout.Label(core.target.targetBody.GetExperimentBiomeSafe(core.target.targetLatitude, core.target.targetLongitude));
GUILayout.EndHorizontal();
}
else
{
if (GUILayout.Button("Enter target coordinates"))
{
core.target.SetPositionTarget(mainBody, core.target.targetLatitude, core.target.targetLongitude);
}
}
if (GUILayout.Button("Pick target on map"))
{
core.target.PickPositionTargetOnMap();
}
List <LandingSite> availableLandingSites = landingSites.Where(p => p.body == mainBody).ToList();
if (availableLandingSites.Any())
{
GUILayout.BeginHorizontal();
landingSiteIdx = GuiUtils.ComboBox.Box(landingSiteIdx, availableLandingSites.Select(p => p.name).ToArray(), this);
if (GUILayout.Button("Set", GUILayout.ExpandWidth(false)))
{
core.target.SetPositionTarget(mainBody, availableLandingSites[landingSiteIdx].latitude, availableLandingSites[landingSiteIdx].longitude);
}
GUILayout.EndHorizontal();
}
DrawGUITogglePredictions();
if (core.landing != null)
{
GUILayout.Label("Autopilot:");
predictor.maxOrbits = core.landing.enabled ? 0.5 : 4;
predictor.noSkipToFreefall = !core.landing.enabled;
if (core.landing.enabled)
{
if (GUILayout.Button("Abort autoland"))
{
core.landing.StopLanding();
}
}
else
{
GUILayout.BeginHorizontal();
if (!core.target.PositionTargetExists || vessel.LandedOrSplashed)
{
GUI.enabled = false;
}
if (GUILayout.Button("Land at target"))
{
core.landing.LandAtPositionTarget(this);
}
GUI.enabled = !vessel.LandedOrSplashed;
if (GUILayout.Button("Land somewhere"))
{
core.landing.LandUntargeted(this);
}
GUI.enabled = true;
GUILayout.EndHorizontal();
}
GuiUtils.SimpleTextBox("Touchdown speed:", core.landing.touchdownSpeed, "m/s", 35);
if (core.landing != null)
{
core.node.autowarp = GUILayout.Toggle(core.node.autowarp, "Auto-warp");
}
core.landing.deployGears = GUILayout.Toggle(core.landing.deployGears, "Deploy Landing Gear");
GuiUtils.SimpleTextBox("Stage Limit:", core.landing.limitGearsStage, "", 35);
core.landing.deployChutes = GUILayout.Toggle(core.landing.deployChutes, "Deploy Parachutes");
predictor.deployChutes = core.landing.deployChutes;
GuiUtils.SimpleTextBox("Stage Limit:", core.landing.limitChutesStage, "", 35);
predictor.limitChutesStage = core.landing.limitChutesStage;
core.landing.rcsAdjustment = GUILayout.Toggle(core.landing.rcsAdjustment, "Use RCS for small adjustment");
if (core.landing.enabled)
{
GUILayout.Label("Status: " + core.landing.status);
GUILayout.Label("Step: " + (core.landing.CurrentStep != null ? core.landing.CurrentStep.GetType().Name : "N/A"));
GUILayout.Label("Mode " + (core.landing.descentSpeedPolicy != null ? core.landing.descentSpeedPolicy.GetType().Name : "N/A") + " (" + core.landing.UseAtmosphereToBrake().ToString() + ")");
//GUILayout.Label("DecEndAlt: " + core.landing.DecelerationEndAltitude().ToString("F2"));
//var dragLength = mainBody.DragLength(core.landing.LandingAltitude, core.landing.vesselAverageDrag, vesselState.mass);
//GUILayout.Label("Drag Length: " + ( dragLength < double.MaxValue ? dragLength.ToString("F2") : "infinite"));
//
//string parachuteInfo = core.landing.ParachuteControlInfo;
//if (null != parachuteInfo)
//{
// GUILayout.Label(parachuteInfo);
//}
}
}
GUILayout.EndVertical();
base.WindowGUI(windowID);
}
protected override void WindowGUI(int windowID)
{
if (!core.target.NormalTargetExists)
{
GUILayout.Label("Select a target to rendezvous with.");
base.WindowGUI(windowID);
return;
}
if (core.target.Orbit.referenceBody != orbit.referenceBody)
{
GUILayout.Label("Rendezvous target must be in the same sphere of influence.");
base.WindowGUI(windowID);
return;
}
GUILayout.BeginVertical();
step = (Step)GuiUtils.ArrowSelector((int)step, numSteps, stepStrings[(int)step]);
double leadTime = 30;
switch (step)
{
case Step.AlignPlanes:
GUILayout.Label("First, bring your relative inclination to zero by aligning your orbital plane with the target's orbital plane:");
GUILayout.Label("Relative inclination: " + orbit.RelativeInclination(core.target.Orbit).ToString("F2") + "º");
if (GUILayout.Button("Align Planes"))
{
double UT;
Vector3d dV;
if (orbit.AscendingNodeExists(core.target.Orbit))
{
dV = OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesAscending(orbit, core.target.Orbit, vesselState.time, out UT);
}
else
{
dV = OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesDescending(orbit, core.target.Orbit, vesselState.time, out UT);
}
vessel.PlaceManeuverNode(orbit, dV, UT);
}
break;
case Step.PhasingOrbit:
double phasingOrbitRadius = 0.9 * core.target.Orbit.PeR;
if (phasingOrbitRadius < orbit.referenceBody.Radius + orbit.referenceBody.RealMaxAtmosphereAltitude())
{
phasingOrbitRadius = 1.1 * core.target.Orbit.ApR;
}
double phasingOrbitAltitude = phasingOrbitRadius - mainBody.Radius;
GUILayout.Label("Next, establish a circular phasing orbit close to the target orbit.");
GUILayout.Label("Target orbit: " + MuUtils.ToSI(core.target.Orbit.PeA, 3) + "m x " + MuUtils.ToSI(core.target.Orbit.ApA, 3) + "m");
GUILayout.Label("Suggested phasing orbit: " + MuUtils.ToSI(phasingOrbitAltitude, 3) + "m x " + MuUtils.ToSI(phasingOrbitAltitude, 3) + "m");
GUILayout.Label("Current orbit: " + MuUtils.ToSI(orbit.PeA, 3) + "m x " + MuUtils.ToSI(orbit.ApA, 3) + "m");
if (GUILayout.Button("Establish Phasing Orbit"))
{
if (orbit.ApR < phasingOrbitRadius)
{
double UT1 = vesselState.time + leadTime;
Vector3d dV1 = OrbitalManeuverCalculator.DeltaVToChangeApoapsis(orbit, UT1, phasingOrbitRadius);
vessel.PlaceManeuverNode(orbit, dV1, UT1);
Orbit transferOrbit = vessel.patchedConicSolver.maneuverNodes[0].nextPatch;
double UT2 = transferOrbit.NextApoapsisTime(UT1);
Vector3d dV2 = OrbitalManeuverCalculator.DeltaVToCircularize(transferOrbit, UT2);
vessel.PlaceManeuverNode(transferOrbit, dV2, UT2);
}
else if (orbit.PeR > phasingOrbitRadius)
{
double UT1 = vesselState.time + leadTime;
Vector3d dV1 = OrbitalManeuverCalculator.DeltaVToChangePeriapsis(orbit, UT1, phasingOrbitRadius);
vessel.PlaceManeuverNode(orbit, dV1, UT1);
Orbit transferOrbit = vessel.patchedConicSolver.maneuverNodes[0].nextPatch;
double UT2 = transferOrbit.NextPeriapsisTime(UT1);
Vector3d dV2 = OrbitalManeuverCalculator.DeltaVToCircularize(transferOrbit, UT2);
vessel.PlaceManeuverNode(transferOrbit, dV2, UT2);
}
else
{
double UT = orbit.NextTimeOfRadius(vesselState.time, phasingOrbitRadius);
Vector3d dV = OrbitalManeuverCalculator.DeltaVToCircularize(orbit, UT);
vessel.PlaceManeuverNode(orbit, dV, UT);
}
}
break;
case Step.Transfer:
GUILayout.Label("Once in the phasing orbit, transfer to the target orbit at just the right time to intercept the target:");
if (GUILayout.Button("Intercept with Hohmann transfer"))
{
double UT;
Vector3d dV = OrbitalManeuverCalculator.DeltaVAndTimeForHohmannTransfer(orbit, core.target.Orbit, vesselState.time, out UT);
vessel.PlaceManeuverNode(orbit, dV, UT);
}
double closestApproachTime = orbit.NextClosestApproachTime(core.target.Orbit, vesselState.time);
GUILayout.Label("Once on a transfer trajectory, match velocities at closest approach:");
GUILayout.Label("Time until closest approach: " + GuiUtils.TimeToDHMS(closestApproachTime - vesselState.time));
GUILayout.Label("Separation at closest approach: " + MuUtils.ToSI(orbit.Separation(core.target.Orbit, closestApproachTime), 0) + "m");
if (GUILayout.Button("Match velocities at closest approach"))
{
double UT = closestApproachTime;
Vector3d dV = OrbitalManeuverCalculator.DeltaVToMatchVelocities(orbit, UT, core.target.Orbit);
vessel.PlaceManeuverNode(orbit, dV, UT);
}
break;
case Step.GetCloser:
GUILayout.Label("If you aren't close enough after matching velocities, thrust gently toward the target:");
if (GUILayout.Button("Get closer"))
{
double UT = vesselState.time;
double interceptUT = UT + 100;
Vector3d dV = OrbitalManeuverCalculator.DeltaVToInterceptAtTime(orbit, UT, core.target.Orbit, interceptUT, 10);
vessel.PlaceManeuverNode(orbit, dV, UT);
}
GUILayout.Label("Then match velocities again at closest approach");
break;
}
GUILayout.EndVertical();
MechJebModuleRendezvousAutopilot autopilot = core.GetComputerModule <MechJebModuleRendezvousAutopilot>();
if (autopilot != null)
{
bool active = GUILayout.Toggle(autopilot.enabled, "Autopilot enable");
if (autopilot.enabled != active)
{
if (active)
{
autopilot.users.Add(this);
}
else
{
autopilot.users.Remove(this);
}
}
if (autopilot.enabled)
{
GUILayout.Label("Status: " + autopilot.status);
}
}
base.WindowGUI(windowID);
}
public override List <ManeuverParameters> MakeNodesImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
if (2 * newSMA > o.Radius(UT) + o.referenceBody.sphereOfInfluence)
{
errorMessage = Localizer.Format("#MechJeb_Sa_errormsg");//Warning: new Semi-Major Axis is very large, and may result in a hyberbolic orbit
}
if (o.Radius(UT) > 2 * newSMA)
{
throw new OperationException(Localizer.Format("#MechJeb_Sa_Exception", o.referenceBody.displayName) + "(" + MuUtils.ToSI(o.referenceBody.Radius, 3) + "m)");//cannot make Semi-Major Axis less than twice the burn altitude plus the radius of <<1>>
}
List <ManeuverParameters> NodeList = new List <ManeuverParameters>();
NodeList.Add(new ManeuverParameters(OrbitalManeuverCalculator.DeltaVForSemiMajorAxis(o, UT, newSMA), UT));
return(NodeList);
}
protected override void WindowGUI(int windowID)
{
GUILayout.BeginVertical();
bool showingGuidance = (core.target.Target != null && core.target.Name == TARGET_NAME);
if (showingGuidance)
{
GUILayout.Label("The purple circle on the navball points along the ascent path.");
if (GUILayout.Button("Stop showing navball guidance"))
{
core.target.Unset();
}
}
else if (GUILayout.Button("Show navball ascent path guidance"))
{
core.target.SetDirectionTarget(TARGET_NAME);
}
if (autopilot != null)
{
if (autopilot.enabled)
{
if (GUILayout.Button("Disengage autopilot"))
{
autopilot.users.Remove(this);
}
}
else
{
if (GUILayout.Button("Engage autopilot"))
{
autopilot.users.Add(this);
}
}
ascentPath = autopilot.ascentPath;
GuiUtils.SimpleTextBox("Orbit altitude", autopilot.desiredOrbitAltitude, "km");
autopilot.desiredInclination = desiredInclination;
}
GuiUtils.SimpleTextBox("Orbit inclination", desiredInclination, "º");
core.thrust.LimitToPreventOverheatsInfoItem();
core.thrust.LimitToTerminalVelocityInfoItem();
core.thrust.LimitAccelerationInfoItem();
core.thrust.LimitThrottleInfoItem();
autopilot.forceRoll = GUILayout.Toggle(autopilot.forceRoll, "Force Roll");
GUILayout.BeginHorizontal();
GUIStyle s = new GUIStyle(GUI.skin.toggle);
if (autopilot.limitingAoA)
{
s.onHover.textColor = s.onNormal.textColor = Color.green;
}
autopilot.limitAoA = GUILayout.Toggle(autopilot.limitAoA, "Limit angle of attack to", s, GUILayout.Width(150));
autopilot.maxAoA.text = GUILayout.TextField(autopilot.maxAoA.text, GUILayout.Width(30));
GUILayout.Label("º", GUILayout.ExpandWidth(false));
GUILayout.EndHorizontal();
if (autopilot.limitAoA)
{
GuiUtils.SimpleTextBox("Dynamic Pressure Fadeout", autopilot.aoALimitFadeoutPressure, "", 50);
}
autopilot.correctiveSteering = GUILayout.Toggle(autopilot.correctiveSteering, "Corrective steering");
autopilot.autostage = GUILayout.Toggle(autopilot.autostage, "Autostage");
if (autopilot.autostage)
{
core.staging.AutostageSettingsInfoItem();
}
core.node.autowarp = GUILayout.Toggle(core.node.autowarp, "Auto-warp");
if (autopilot != null && vessel.LandedOrSplashed)
{
if (core.target.NormalTargetExists)
{
if (core.node.autowarp)
{
GUILayout.BeginHorizontal();
GUILayout.Label("Launch countdown:", GUILayout.ExpandWidth(true));
autopilot.warpCountDown.text = GUILayout.TextField(autopilot.warpCountDown.text, GUILayout.Width(60));
GUILayout.Label("s", GUILayout.ExpandWidth(false));
GUILayout.EndHorizontal();
}
if (!launchingToPlane && !launchingToRendezvous && !launchingToInterplanetary)
{
GUILayout.BeginHorizontal();
if (GUILayout.Button("Launch to rendezvous:", GUILayout.ExpandWidth(false)))
{
launchingToRendezvous = true;
lastTMinus = 999;
}
autopilot.launchPhaseAngle.text = GUILayout.TextField(autopilot.launchPhaseAngle.text, GUILayout.Width(60));
GUILayout.Label("º", GUILayout.ExpandWidth(false));
GUILayout.EndHorizontal();
if (GUILayout.Button("Launch into plane of target"))
{
launchingToPlane = true;
lastTMinus = 999;
}
if (core.target.TargetOrbit.referenceBody == orbit.referenceBody.referenceBody)
{
if (GUILayout.Button("Launch at interplanetary window"))
{
launchingToInterplanetary = true;
lastTMinus = 999;
//compute the desired launch date
OrbitalManeuverCalculator.DeltaVAndTimeForHohmannTransfer(mainBody.orbit, core.target.TargetOrbit, vesselState.time, out interplanetaryWindowUT);
double desiredOrbitPeriod = 2 * Math.PI * Math.Sqrt(Math.Pow(mainBody.Radius + autopilot.desiredOrbitAltitude, 3) / mainBody.gravParameter);
//launch just before the window, but don't try to launch in the past
interplanetaryWindowUT -= 3 * desiredOrbitPeriod;
interplanetaryWindowUT = Math.Max(vesselState.time + autopilot.warpCountDown, interplanetaryWindowUT);
}
}
}
}
else
{
launchingToInterplanetary = launchingToPlane = launchingToRendezvous = false;
GUILayout.Label("Select a target for a timed launch.");
}
if (launchingToInterplanetary || launchingToPlane || launchingToRendezvous)
{
double tMinus = 0;
string message = "";
if (launchingToInterplanetary)
{
tMinus = interplanetaryWindowUT - vesselState.time;
message = "Launching at interplanetary window";
}
else if (launchingToPlane)
{
tMinus = LaunchTiming.TimeToPlane(mainBody, vesselState.latitude, vesselState.longitude, core.target.TargetOrbit);
desiredInclination = core.target.TargetOrbit.inclination;
desiredInclination *= Math.Sign(Vector3d.Dot(core.target.TargetOrbit.SwappedOrbitNormal(), Vector3d.Cross(vesselState.CoM - mainBody.position, mainBody.transform.up)));
message = "Launching to target plane";
}
else if (launchingToRendezvous)
{
tMinus = LaunchTiming.TimeToPhaseAngle(autopilot.launchPhaseAngle, mainBody, vesselState.longitude, core.target.TargetOrbit);
message = "Launching to rendezvous";
}
double launchTime = vesselState.time + tMinus;
if (tMinus < 3 * vesselState.deltaT || (tMinus > 10.0 && lastTMinus < 1.0))
{
if (autopilot.enabled)
{
Staging.ActivateNextStage();
}
launchingToInterplanetary = launchingToPlane = launchingToRendezvous = false;
}
else
{
message += ": T-" + MuUtils.ToSI(tMinus, 0) + "s";
if (autopilot.enabled && core.node.autowarp)
{
core.warp.WarpToUT(launchTime - autopilot.warpCountDown);
}
}
GUILayout.Label(message);
lastTMinus = tMinus;
if (GUILayout.Button("Abort"))
{
launchingToInterplanetary = launchingToPlane = launchingToRendezvous = false;
}
}
}
if (autopilot != null && autopilot.enabled)
{
GUILayout.Label("Autopilot status: " + autopilot.status);
}
MechJebModuleAscentPathEditor editor = core.GetComputerModule <MechJebModuleAscentPathEditor>();
if (editor != null)
{
editor.enabled = GUILayout.Toggle(editor.enabled, "Edit ascent path");
}
GUILayout.EndVertical();
base.WindowGUI(windowID);
}
protected override void WindowGUI(int windowID)
{
GUILayout.BeginVertical();
bool showingGuidance = (core.target.Target != null && core.target.Name == TARGET_NAME);
if (showingGuidance)
{
GUILayout.Label("The purple circle on the navball points along the ascent path.");
if (GUILayout.Button("Stop showing navball guidance"))
{
core.target.Unset();
}
}
else if (GUILayout.Button("Show navball ascent path guidance"))
{
core.target.SetDirectionTarget(TARGET_NAME);
}
if (autopilot != null)
{
if (autopilot.enabled)
{
if (GUILayout.Button("Disengage autopilot"))
{
autopilot.users.Remove(this);
}
}
else
{
if (GUILayout.Button("Engage autopilot"))
{
autopilot.users.Add(this);
}
}
ascentPath = autopilot.ascentPath;
GuiUtils.SimpleTextBox("Orbit altitude", autopilot.desiredOrbitAltitude, "km");
autopilot.desiredInclination = desiredInclination;
}
GuiUtils.SimpleTextBox("Orbit inclination", desiredInclination, "º");
core.thrust.limitToPreventOverheats = GUILayout.Toggle(core.thrust.limitToPreventOverheats, "Prevent overheats");
core.thrust.limitToTerminalVelocity = GUILayout.Toggle(core.thrust.limitToTerminalVelocity, "Limit to terminal velocity");
GUILayout.BeginHorizontal();
core.thrust.limitAcceleration = GUILayout.Toggle(core.thrust.limitAcceleration, "Limit acceleration to", GUILayout.ExpandWidth(false));
core.thrust.maxAcceleration.text = GUILayout.TextField(core.thrust.maxAcceleration.text, GUILayout.ExpandWidth(true));
GUILayout.Label("m/s²", GUILayout.ExpandWidth(false));
GUILayout.EndHorizontal();
autopilot.correctiveSteering = GUILayout.Toggle(autopilot.correctiveSteering, "Corrective steering");
core.staging.AutostageInfoItem();
core.node.autowarp = GUILayout.Toggle(core.node.autowarp, "Auto-warp");
if (autopilot != null && vessel.LandedOrSplashed)
{
if (core.target.NormalTargetExists)
{
if (!launchingToPlane && !launchingToRendezvous)
{
GUILayout.BeginHorizontal();
if (GUILayout.Button("Launch to rendezvous:", GUILayout.ExpandWidth(false)))
{
launchingToRendezvous = true;
}
autopilot.launchPhaseAngle.text = GUILayout.TextField(autopilot.launchPhaseAngle.text, GUILayout.Width(60));
GUILayout.Label("º", GUILayout.ExpandWidth(false));
GUILayout.EndHorizontal();
}
if (!launchingToPlane && !launchingToRendezvous && GUILayout.Button("Launch into plane of target"))
{
launchingToPlane = true;
}
}
else
{
launchingToPlane = launchingToRendezvous = false;
GUILayout.Label("Select a target for a timed launch.");
}
if (launchingToPlane || launchingToRendezvous)
{
double tMinus;
if (launchingToPlane)
{
tMinus = LaunchTiming.TimeToPlane(mainBody, vesselState.latitude, vesselState.longitude, core.target.Orbit);
}
else
{
tMinus = LaunchTiming.TimeToPhaseAngle(autopilot.launchPhaseAngle, mainBody, vesselState.longitude, core.target.Orbit);
}
double launchTime = vesselState.time + tMinus;
core.warp.WarpToUT(launchTime);
if (launchingToPlane)
{
desiredInclination = core.target.Orbit.inclination;
desiredInclination *= Math.Sign(Vector3d.Dot(core.target.Orbit.SwappedOrbitNormal(), Vector3d.Cross(vesselState.CoM - mainBody.position, mainBody.transform.up)));
}
if (autopilot.enabled)
{
core.warp.WarpToUT(launchTime);
}
GUILayout.Label("Launching to " + (launchingToPlane ? "target plane" : "rendezvous") + ": T-" + MuUtils.ToSI(tMinus, 0) + "s");
if (tMinus < 3 * vesselState.deltaT)
{
if (autopilot.enabled)
{
Staging.ActivateNextStage();
}
launchingToPlane = launchingToRendezvous = false;
}
if (GUILayout.Button("Abort"))
{
launchingToPlane = launchingToRendezvous = false;
}
}
if (autopilot.enabled)
{
GUILayout.Label("Autopilot status: " + autopilot.status);
}
}
MechJebModuleAscentPathEditor editor = core.GetComputerModule <MechJebModuleAscentPathEditor>();
if (editor != null)
{
editor.enabled = GUILayout.Toggle(editor.enabled, "Edit ascent path");
}
GUILayout.EndVertical();
base.WindowGUI(windowID);
}
public override void Drive(FlightCtrlState s)
{
if (!core.target.NormalTargetExists)
{
users.Clear();
return;
}
core.node.autowarp = core.target.Distance > 1000; //don't warp when close to target, because warping introduces small perturbations
//If we get within the target distance and then next maneuver node is still
//far in the future, delete it and we will create a new one to match velocities immediately.
//This can often happen because the target vessel's orbit shifts slightly when it is unpacked.
if (core.target.Distance < desiredDistance &&
vessel.patchedConicSolver.maneuverNodes.Count > 0 &&
vessel.patchedConicSolver.maneuverNodes[0].UT > vesselState.time + 1)
{
vessel.RemoveAllManeuverNodes();
}
if (vessel.patchedConicSolver.maneuverNodes.Count > 0)
{
//If we have plotted a maneuver, execute it.
if (!core.node.enabled)
{
core.node.ExecuteAllNodes(this);
}
}
else if (core.target.Distance < desiredDistance * 1.05 + 2 &&
core.target.RelativeVelocity.magnitude < 1)
{
//finished
users.Clear();
core.thrust.ThrustOff();
status = "Successful rendezvous";
}
else if (core.target.Distance < desiredDistance * 1.05 + 2)
{
//We are within the target distance: match velocities
double UT = vesselState.time;
Vector3d dV = OrbitalManeuverCalculator.DeltaVToMatchVelocities(orbit, UT, core.target.Orbit);
vessel.PlaceManeuverNode(orbit, dV, UT);
status = "Within " + desiredDistance.ToString() + "m: matching velocities.";
}
else if (core.target.Distance < vesselState.radius / 25)
{
if (orbit.NextClosestApproachDistance(core.target.Orbit, vesselState.time) < desiredDistance &&
orbit.NextClosestApproachTime(core.target.Orbit, vesselState.time) < vesselState.time + 150)
{
//We're close to the target, and on a course that will take us closer. Kill relvel at closest approach
double UT = orbit.NextClosestApproachTime(core.target.Orbit, vesselState.time);
Vector3d dV = OrbitalManeuverCalculator.DeltaVToMatchVelocities(orbit, UT, core.target.Orbit);
//adjust burn time so as to come to rest at the desired distance from the target:
double approachDistance = orbit.Separation(core.target.Orbit, UT);
double approachSpeed = (orbit.SwappedOrbitalVelocityAtUT(UT) - core.target.Orbit.SwappedOrbitalVelocityAtUT(UT)).magnitude;
if (approachDistance < desiredDistance)
{
UT -= Math.Sqrt(Math.Abs(desiredDistance * desiredDistance - approachDistance * approachDistance)) / approachSpeed;
}
//if coming in hot, stop early to avoid crashing:
if (approachSpeed > 10)
{
UT -= 1;
}
vessel.PlaceManeuverNode(orbit, dV, UT);
status = "Planning to match velocities at closest approach.";
}
else
{
//We're not far from the target. Close the distance
double closingSpeed = core.target.Distance / 100;
if (closingSpeed > 100)
{
closingSpeed = 100;
}
double closingTime = core.target.Distance / closingSpeed;
double UT = vesselState.time + 15;
double interceptUT = UT + closingTime;
Vector3d dV = OrbitalManeuverCalculator.DeltaVToInterceptAtTime(orbit, UT, core.target.Orbit, interceptUT, 0);
vessel.PlaceManeuverNode(orbit, dV, UT);
status = "Close to target: plotting intercept";
}
}
else if (orbit.NextClosestApproachDistance(core.target.Orbit, vesselState.time) < core.target.Orbit.semiMajorAxis / 25)
{
//We're not close to the target, but we're on an approximate intercept course.
//Kill relative velocities at closest approach
double UT = orbit.NextClosestApproachTime(core.target.Orbit, vesselState.time);
Vector3d dV = OrbitalManeuverCalculator.DeltaVToMatchVelocities(orbit, UT, core.target.Orbit);
//adjust burn time so as to come to rest at the desired distance from the target:
double approachDistance = (orbit.SwappedAbsolutePositionAtUT(UT) - core.target.Orbit.SwappedAbsolutePositionAtUT(UT)).magnitude;
double approachSpeed = (orbit.SwappedOrbitalVelocityAtUT(UT) - core.target.Orbit.SwappedOrbitalVelocityAtUT(UT)).magnitude;
if (approachDistance < desiredDistance)
{
UT -= Math.Sqrt(Math.Abs(desiredDistance * desiredDistance - approachDistance * approachDistance)) / approachSpeed;
}
//if coming in hot, stop early to avoid crashing:
if (approachSpeed > 10)
{
UT -= 1;
}
vessel.PlaceManeuverNode(orbit, dV, UT);
status = "On intercept course. Planning to match velocities at closest approach.";
}
else if (orbit.RelativeInclination(core.target.Orbit) < 0.05 && orbit.eccentricity < 0.05 && orbit.SynodicPeriod(core.target.Orbit) < 5 * orbit.period)
{
//We're not on an intercept course, but we have a circular orbit in the right plane.
//Also we are phasing quickly enough that it won't be too long until an intercept window
//Plot a Hohmann transfer intercept.
double UT;
Vector3d dV = OrbitalManeuverCalculator.DeltaVAndTimeForHohmannTransfer(orbit, core.target.Orbit, vesselState.time, out UT);
vessel.PlaceManeuverNode(orbit, dV, UT);
status = "Planning Hohmann transfer for intercept.";
}
else if (orbit.RelativeInclination(core.target.Orbit) < 0.05 && orbit.eccentricity < 0.05)
{
//We are in a circular orbit in the right plane, but we aren't phasing quickly enough. Move to a better phasing orbit
double lowPhasingRadius = core.target.Orbit.semiMajorAxis / 1.16;
double highPhasingRadius = core.target.Orbit.semiMajorAxis * 1.16;
bool useLowPhasingRadius = (lowPhasingRadius > mainBody.RealMaxAtmosphereAltitude() + 3000 && orbit.semiMajorAxis < core.target.orbit.semiMajorAxis);
double phasingOrbitRadius = (useLowPhasingRadius ? lowPhasingRadius : highPhasingRadius);
if (orbit.ApR < phasingOrbitRadius)
{
double UT1 = vesselState.time + 15;
Vector3d dV1 = OrbitalManeuverCalculator.DeltaVToChangeApoapsis(orbit, UT1, phasingOrbitRadius);
vessel.PlaceManeuverNode(orbit, dV1, UT1);
Orbit transferOrbit = vessel.patchedConicSolver.maneuverNodes[0].nextPatch;
double UT2 = transferOrbit.NextApoapsisTime(UT1);
Vector3d dV2 = OrbitalManeuverCalculator.DeltaVToCircularize(transferOrbit, UT2);
vessel.PlaceManeuverNode(transferOrbit, dV2, UT2);
}
else if (orbit.PeR > phasingOrbitRadius)
{
double UT1 = vesselState.time + 15;
Vector3d dV1 = OrbitalManeuverCalculator.DeltaVToChangePeriapsis(orbit, UT1, phasingOrbitRadius);
vessel.PlaceManeuverNode(orbit, dV1, UT1);
Orbit transferOrbit = vessel.patchedConicSolver.maneuverNodes[0].nextPatch;
double UT2 = transferOrbit.NextPeriapsisTime(UT1);
Vector3d dV2 = OrbitalManeuverCalculator.DeltaVToCircularize(transferOrbit, UT2);
vessel.PlaceManeuverNode(transferOrbit, dV2, UT2);
}
else
{
double UT = orbit.NextTimeOfRadius(vesselState.time, phasingOrbitRadius);
Vector3d dV = OrbitalManeuverCalculator.DeltaVToCircularize(orbit, UT);
vessel.PlaceManeuverNode(orbit, dV, UT);
}
status = "Increasing phasing rate by establishing new phasing orbit at " + MuUtils.ToSI(phasingOrbitRadius - mainBody.Radius, 0) + "m";
}
else if (orbit.RelativeInclination(core.target.Orbit) < 0.05)
{
//We're not on an intercept course. We're in the right plane, but our orbit isn't circular. Circularize.
bool circularizeAtPe;
if (orbit.eccentricity > 1)
{
circularizeAtPe = true;
}
else
{
circularizeAtPe = Math.Abs(orbit.PeR - core.target.Orbit.semiMajorAxis) < Math.Abs(orbit.ApR - core.target.Orbit.semiMajorAxis);
}
double UT;
if (circularizeAtPe)
{
UT = Math.Max(vesselState.time, orbit.NextPeriapsisTime(vesselState.time));
}
else
{
UT = orbit.NextApoapsisTime(vesselState.time);
}
Vector3d dV = OrbitalManeuverCalculator.DeltaVToCircularize(orbit, UT);
vessel.PlaceManeuverNode(orbit, dV, UT);
status = "Circularizing.";
}
else
{
//We're not on an intercept course, and we're not in the right plane. Match planes
bool ascending;
if (orbit.eccentricity < 1)
{
if (orbit.TimeOfAscendingNode(core.target.Orbit, vesselState.time) < orbit.TimeOfDescendingNode(core.target.Orbit, vesselState.time))
{
ascending = true;
}
else
{
ascending = false;
}
}
else
{
if (orbit.AscendingNodeExists(core.target.Orbit))
{
ascending = true;
}
else
{
ascending = false;
}
}
double UT;
Vector3d dV;
if (ascending)
{
dV = OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesAscending(orbit, core.target.Orbit, vesselState.time, out UT);
}
else
{
dV = OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesDescending(orbit, core.target.Orbit, vesselState.time, out UT);
}
vessel.PlaceManeuverNode(orbit, dV, UT);
status = "Matching planes.";
}
}
protected override void WindowGUI(int windowID)
{
if (!core.target.NormalTargetExists)
{
GUILayout.Label(Localizer.Format("#MechJeb_RZplan_label1"));//"Select a target to rendezvous with."
base.WindowGUI(windowID);
return;
}
if (core.target.TargetOrbit.referenceBody != orbit.referenceBody)
{
GUILayout.Label(Localizer.Format("#MechJeb_RZplan_label2"));//"Rendezvous target must be in the same sphere of influence."
base.WindowGUI(windowID);
return;
}
GUILayout.BeginVertical();
//Information readouts:
GuiUtils.SimpleLabel(Localizer.Format("#MechJeb_RZplan_label3"), core.target.Name);//"Rendezvous target"
const double leadTime = 30;
GuiUtils.SimpleLabel(Localizer.Format("#MechJeb_RZplan_label4"), MuUtils.ToSI(core.target.TargetOrbit.PeA, 3) + "m x " + MuUtils.ToSI(core.target.TargetOrbit.ApA, 3) + "m"); //"Target orbit"
GuiUtils.SimpleLabel(Localizer.Format("#MechJeb_RZplan_label5"), MuUtils.ToSI(orbit.PeA, 3) + "m x " + MuUtils.ToSI(orbit.ApA, 3) + "m"); //"Current orbit"
GuiUtils.SimpleLabel(Localizer.Format("#MechJeb_RZplan_label6"), orbit.RelativeInclination(core.target.TargetOrbit).ToString("F2") + "º"); //"Relative inclination"
double closestApproachTime = orbit.NextClosestApproachTime(core.target.TargetOrbit, vesselState.time);
GuiUtils.SimpleLabel(Localizer.Format("#MechJeb_RZplan_label7"), GuiUtils.TimeToDHMS(closestApproachTime - vesselState.time)); //"Time until closest approach"
GuiUtils.SimpleLabel(Localizer.Format("#MechJeb_RZplan_label8"), MuUtils.ToSI(orbit.Separation(core.target.TargetOrbit, closestApproachTime), 0) + "m"); //"Separation at closest approach"
//Maneuver planning buttons:
if (GUILayout.Button(Localizer.Format("#MechJeb_RZplan_button1")))//"Align Planes"
{
double UT;
Vector3d dV;
if (orbit.AscendingNodeExists(core.target.TargetOrbit))
{
dV = OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesAscending(orbit, core.target.TargetOrbit, vesselState.time, out UT);
}
else
{
dV = OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesDescending(orbit, core.target.TargetOrbit, vesselState.time, out UT);
}
vessel.RemoveAllManeuverNodes();
vessel.PlaceManeuverNode(orbit, dV, UT);
}
GUILayout.BeginHorizontal();
if (GUILayout.Button(Localizer.Format("#MechJeb_RZplan_button2")))//"Establish new orbit at"
{
double phasingOrbitRadius = phasingOrbitAltitude + mainBody.Radius;
vessel.RemoveAllManeuverNodes();
if (orbit.ApR < phasingOrbitRadius)
{
double UT1 = vesselState.time + leadTime;
Vector3d dV1 = OrbitalManeuverCalculator.DeltaVToChangeApoapsis(orbit, UT1, phasingOrbitRadius);
vessel.PlaceManeuverNode(orbit, dV1, UT1);
Orbit transferOrbit = vessel.patchedConicSolver.maneuverNodes[0].nextPatch;
double UT2 = transferOrbit.NextApoapsisTime(UT1);
Vector3d dV2 = OrbitalManeuverCalculator.DeltaVToCircularize(transferOrbit, UT2);
vessel.PlaceManeuverNode(transferOrbit, dV2, UT2);
}
else if (orbit.PeR > phasingOrbitRadius)
{
double UT1 = vesselState.time + leadTime;
Vector3d dV1 = OrbitalManeuverCalculator.DeltaVToChangePeriapsis(orbit, UT1, phasingOrbitRadius);
vessel.PlaceManeuverNode(orbit, dV1, UT1);
Orbit transferOrbit = vessel.patchedConicSolver.maneuverNodes[0].nextPatch;
double UT2 = transferOrbit.NextPeriapsisTime(UT1);
Vector3d dV2 = OrbitalManeuverCalculator.DeltaVToCircularize(transferOrbit, UT2);
vessel.PlaceManeuverNode(transferOrbit, dV2, UT2);
}
else
{
double UT = orbit.NextTimeOfRadius(vesselState.time, phasingOrbitRadius);
Vector3d dV = OrbitalManeuverCalculator.DeltaVToCircularize(orbit, UT);
vessel.PlaceManeuverNode(orbit, dV, UT);
}
}
phasingOrbitAltitude.text = GUILayout.TextField(phasingOrbitAltitude.text, GUILayout.Width(70));
GUILayout.Label("km", GUILayout.ExpandWidth(false));
GUILayout.EndHorizontal();
if (GUILayout.Button(Localizer.Format("#MechJeb_RZplan_button3")))//"Intercept with Hohmann transfer"
{
double UT;
Vector3d dV = OrbitalManeuverCalculator.DeltaVAndTimeForHohmannTransfer(orbit, core.target.TargetOrbit, vesselState.time, out UT);
vessel.RemoveAllManeuverNodes();
vessel.PlaceManeuverNode(orbit, dV, UT);
}
if (GUILayout.Button(Localizer.Format("#MechJeb_RZplan_button4")))//"Match velocities at closest approach"
{
double UT = closestApproachTime;
Vector3d dV = OrbitalManeuverCalculator.DeltaVToMatchVelocities(orbit, UT, core.target.TargetOrbit);
vessel.RemoveAllManeuverNodes();
vessel.PlaceManeuverNode(orbit, dV, UT);
}
if (GUILayout.Button(Localizer.Format("#MechJeb_RZplan_button5")))//"Get closer"
{
double UT = vesselState.time;
Vector3d dV = OrbitalManeuverCalculator.DeltaVToInterceptAtTime(orbit, UT, core.target.TargetOrbit, 100, 10);
vessel.RemoveAllManeuverNodes();
vessel.PlaceManeuverNode(orbit, dV, UT);
}
if (core.node != null)
{
if (vessel.patchedConicSolver.maneuverNodes.Any() && !core.node.enabled)
{
if (GUILayout.Button(Localizer.Format("#MechJeb_RZplan_button6")))//"Execute next node"
{
core.node.ExecuteOneNode(this);
}
if (vessel.patchedConicSolver.maneuverNodes.Count > 1)
{
if (GUILayout.Button(Localizer.Format("#MechJeb_RZplan_button7")))//"Execute all nodes"
{
core.node.ExecuteAllNodes(this);
}
}
}
else if (core.node.enabled)
{
if (GUILayout.Button(Localizer.Format("#MechJeb_RZplan_button8")))//"Abort node execution"
{
core.node.Abort();
}
}
GUILayout.BeginHorizontal();
core.node.autowarp = GUILayout.Toggle(core.node.autowarp, Localizer.Format("#MechJeb_RZplan_checkbox"), GUILayout.ExpandWidth(true)); //"Auto-warp"
GUILayout.Label(Localizer.Format("#MechJeb_RZplan_label9"), GUILayout.ExpandWidth(false)); //"Tolerance:"
core.node.tolerance.text = GUILayout.TextField(core.node.tolerance.text, GUILayout.Width(35), GUILayout.ExpandWidth(false));
if (GUILayout.Button("+", GUILayout.ExpandWidth(false)))
{
core.node.tolerance.val += 0.1;
}
if (GUILayout.Button("-", GUILayout.ExpandWidth(false)))
{
core.node.tolerance.val -= core.node.tolerance.val > 0.1 ? 0.1 : 0.0;
}
if (GUILayout.Button("R", GUILayout.ExpandWidth(false)))
{
core.node.tolerance.val = 0.1;
}
GUILayout.Label("m/s", GUILayout.ExpandWidth(false));
GUILayout.EndHorizontal();
}
GUILayout.EndVertical();
base.WindowGUI(windowID);
}
