public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
if (!target.NormalTargetExists)
{
throw new OperationException("must select a target to match planes with.");
}
else if (o.referenceBody != target.TargetOrbit.referenceBody)
{
throw new OperationException("can only match planes with an object in the same sphere of influence.");
}
else if (timeSelector.timeReference == TimeReference.REL_ASCENDING)
{
if (!o.AscendingNodeExists(target.TargetOrbit))
{
throw new OperationException("ascending node with target doesn't exist.");
}
}
else
{
if (!o.DescendingNodeExists(target.TargetOrbit))
{
throw new OperationException("descending node with target doesn't exist.");
}
}
Vector3d dV = (timeSelector.timeReference == TimeReference.REL_ASCENDING) ?
OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesAscending(o, target.TargetOrbit, UT, out UT):
OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesDescending(o, target.TargetOrbit, UT, out UT);
return new ManeuverParameters(dV, UT);
}
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("new apoapsis cannot be lower than the altitude of the burn (" + burnAltitude + ")");
}
return new ManeuverParameters(OrbitalManeuverCalculator.DeltaVToChangeApoapsis(o, UT, newApA + o.referenceBody.Radius), UT);
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
if (!target.NormalTargetExists)
throw new OperationException("must select a target to match velocities with.");
else if (o.referenceBody != target.TargetOrbit.referenceBody)
throw new OperationException("target must be in the same sphere of influence.");
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
var dV = OrbitalManeuverCalculator.DeltaVToMatchVelocities(o, UT, target.TargetOrbit);
return new ManeuverParameters(dV, UT);
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
if (2*newSMA > o.Radius(UT) + o.referenceBody.sphereOfInfluence)
{
errorMessage = "Warning: new Semi-Major Axis is very large, and may result in a hyberbolic orbit";
}
if(o.Radius(UT) > 2*newSMA)
{
throw new OperationException("cannot make Semi-Major Axis less than twice the burn altitude plus the radius of " + o.referenceBody.theName + "(" + MuUtils.ToSI(o.referenceBody.Radius, 3) + "m)");
}
return new ManeuverParameters(OrbitalManeuverCalculator.DeltaVForSemiMajorAxis (o, UT, newSMA), UT);
}
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("new periapsis cannot be higher than the altitude of the burn (" + burnAltitude + ")");
}
else if (o.referenceBody.Radius + newApA < o.Radius(UT))
{
throw new OperationException("new apoapsis cannot be lower than the altitude of the burn (" + burnAltitude + ")");
}
else if (newPeA < -o.referenceBody.Radius)
{
throw new OperationException("new periapsis cannot be lower than minus the radius of " + o.referenceBody.theName + "(-" + MuUtils.ToSI(o.referenceBody.Radius, 3) + "m)");
}
return new ManeuverParameters(OrbitalManeuverCalculator.DeltaVToEllipticize(o, UT, newPeA + o.referenceBody.Radius, newApA + o.referenceBody.Radius), UT);
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
return new ManeuverParameters(OrbitalManeuverCalculator.DeltaVToChangeInclination(o, UT, newInc), UT);
}
public override void DoParametersGUI(Orbit o, double universalTime, MechJebModuleTargetController target)
{
GuiUtils.SimpleTextBox("New inclination:", newInc, "º");
timeSelector.DoChooseTimeGUI();
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
if (!target.NormalTargetExists)
{
throw new OperationException("must select a target to match planes with.");
}
else if (o.referenceBody != target.TargetOrbit.referenceBody)
{
throw new OperationException("can only match planes with an object in the same sphere of influence.");
}
var anExists = o.AscendingNodeExists(target.TargetOrbit);
var dnExists = o.DescendingNodeExists(target.TargetOrbit);
double anTime = 0;
double dnTime = 0;
var anDeltaV = anExists ? OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesAscending(o, target.TargetOrbit, UT, out anTime) : Vector3d.zero;
var dnDeltaV = anExists ? OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesDescending(o, target.TargetOrbit, UT, out dnTime) : Vector3d.zero;
Vector3d dV;
if (timeSelector.timeReference == TimeReference.REL_ASCENDING)
{
if (!anExists)
{
throw new OperationException("ascending node with target doesn't exist.");
}
UT = anTime;
dV = anDeltaV;
}
else if (timeSelector.timeReference == TimeReference.REL_DESCENDING)
{
if (!dnExists)
{
throw new OperationException("descending node with target doesn't exist.");
}
UT = dnTime;
dV = dnDeltaV;
}
else if (timeSelector.timeReference == TimeReference.REL_NEAREST_AD)
{
if (!anExists && !dnExists)
{
throw new OperationException("neither ascending nor descending node with target exists.");
}
if (!dnExists || anTime <= dnTime)
{
UT = anTime;
dV = anDeltaV;
}
else
{
UT = dnTime;
dV = dnDeltaV;
}
}
else if (timeSelector.timeReference == TimeReference.REL_HIGHEST_AD)
{
if (!anExists && !dnExists)
{
throw new OperationException("neither ascending nor descending node with target exists.");
}
if (!dnExists || anDeltaV.magnitude <= dnDeltaV.magnitude)
{
UT = anTime;
dV = anDeltaV;
}
else
{
UT = dnTime;
dV = dnDeltaV;
}
}
else
{
throw new OperationException("wrong time reference.");
}
return(new ManeuverParameters(dV, UT));
}
public override void DoParametersGUI(Orbit o, double universalTime, MechJebModuleTargetController target)
{
timeSelector.DoChooseTimeGUI();
}
protected override void LateUpdate()
{
if (shutdown)
{
return;
}
if (!HighLogic.LoadedSceneIsFlight || !FlightGlobals.ready)
{
return;
}
if (SCANcontroller.controller == null)
{
way = null;
return;
}
if (!SCANcontroller.controller.mechJebTargetSelection)
{
way = null;
return;
}
v = FlightGlobals.ActiveVessel;
if (v == null)
{
SCANcontroller.controller.MechJebLoaded = false;
way = null;
return;
}
if (v.mainBody != SCANcontroller.controller.LandingTargetBody)
{
SCANcontroller.controller.LandingTargetBody = v.mainBody;
}
data = SCANUtil.getData(v.mainBody);
if (data == null)
{
SCANcontroller.controller.MechJebLoaded = false;
way = null;
return;
}
if (v.FindPartModulesImplementing <MechJebCore>().Count <= 0)
{
SCANcontroller.controller.MechJebLoaded = false;
way = null;
return;
}
core = v.GetMasterMechJeb();
if (core == null)
{
SCANcontroller.controller.MechJebLoaded = false;
way = null;
return;
}
if (HighLogic.CurrentGame.Mode != Game.Modes.SANDBOX)
{
if (guidanceModule == null)
{
guidanceModule = (DisplayModule)core.GetComputerModule("MechJebModuleLandingGuidance");
}
if (guidanceModule == null)
{
SCANcontroller.controller.MechJebLoaded = false;
way = null;
return;
}
if (!guidanceModule.unlockChecked)
{
return;
}
if (guidanceModule.hidden)
{
SCANcontroller.controller.MechJebLoaded = false;
shutdown = true;
way = null;
return;
}
}
target = core.target;
if (target == null)
{
SCANcontroller.controller.MechJebLoaded = false;
way = null;
return;
}
if (!SCANcontroller.controller.MechJebLoaded)
{
SCANcontroller.controller.MechJebLoaded = true;
RenderingManager.AddToPostDrawQueue(1, drawTarget);
}
if (SCANcontroller.controller.LandingTarget != null)
{
way = SCANcontroller.controller.LandingTarget;
}
if (SCANcontroller.controller.TargetSelecting)
{
way = null;
selectingTarget = true;
if (SCANcontroller.controller.TargetSelectingActive)
{
selectingInMap = true;
}
else
{
selectingInMap = false;
}
coords = SCANcontroller.controller.LandingTargetCoords;
return;
}
else if (selectingTarget)
{
selectingTarget = false;
if (selectingInMap)
{
selectingInMap = false;
coords = SCANcontroller.controller.LandingTargetCoords;
way = new SCANwaypoint(coords.y, coords.x, siteName);
target.SetPositionTarget(SCANcontroller.controller.LandingTargetBody, way.Latitude, way.Longitude);
}
}
selectingInMap = false;
selectingTarget = false;
if (target.Target == null)
{
way = null;
return;
}
if (target.targetBody != v.mainBody)
{
way = null;
return;
}
if (!(target.Target is PositionTarget))
{
way = null;
return;
}
coords.x = target.targetLongitude;
coords.y = target.targetLatitude;
if (way != null)
{
if (!SCANUtil.ApproxEq(coords.x, way.Longitude) || !SCANUtil.ApproxEq(coords.y, way.Latitude))
{
way = new SCANwaypoint(coords.y, coords.x, siteName);
SCANcontroller.controller.LandingTarget = way;
data.addToWaypoints();
}
}
else
{
way = new SCANwaypoint(coords.y, coords.x, siteName);
SCANcontroller.controller.LandingTarget = way;
data.addToWaypoints();
}
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
if (!target.NormalTargetExists)
{
throw new OperationException("must select a target to match planes with.");
}
else if (o.referenceBody != target.TargetOrbit.referenceBody)
{
throw new OperationException("can only match planes with an object in the same sphere of influence.");
}
var anExists = o.AscendingNodeExists(target.TargetOrbit);
var dnExists = o.DescendingNodeExists(target.TargetOrbit);
double anTime = 0;
double dnTime = 0;
var anDeltaV = anExists ? OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesAscending(o, target.TargetOrbit, UT, out anTime) : Vector3d.zero;
var dnDeltaV = anExists ? OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesDescending(o, target.TargetOrbit, UT, out dnTime) : Vector3d.zero;
Vector3d dV;
if(timeSelector.timeReference == TimeReference.REL_ASCENDING)
{
if(!anExists)
{
throw new OperationException("ascending node with target doesn't exist.");
}
UT = anTime;
dV = anDeltaV;
}
else if(timeSelector.timeReference == TimeReference.REL_DESCENDING)
{
if(!dnExists)
{
throw new OperationException("descending node with target doesn't exist.");
}
UT = dnTime;
dV = dnDeltaV;
}
else if(timeSelector.timeReference == TimeReference.REL_NEAREST_AD)
{
if(!anExists && !dnExists)
{
throw new OperationException("neither ascending nor descending node with target exists.");
}
if(!dnExists || anTime <= dnTime)
{
UT = anTime;
dV = anDeltaV;
}
else
{
UT = dnTime;
dV = dnDeltaV;
}
}
else if(timeSelector.timeReference == TimeReference.REL_HIGHEST_AD)
{
if(!anExists && !dnExists)
{
throw new OperationException("neither ascending nor descending node with target exists.");
}
if(!dnExists || anDeltaV.magnitude <= dnDeltaV.magnitude)
{
UT = anTime;
dV = anDeltaV;
}
else
{
UT = dnTime;
dV = dnDeltaV;
}
}
else
{
throw new OperationException("wrong time reference.");
}
return new ManeuverParameters(dV, UT);
}
public override void DoParametersGUI(Orbit o, double universalTime, MechJebModuleTargetController target)
{
GuiUtils.SimpleTextBox("New periapsis:", newPeA, "km");
GuiUtils.SimpleTextBox("New apoapsis:", newApA, "km");
timeSelector.DoChooseTimeGUI();
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
if (2 * newSMA > o.Radius(UT) + o.referenceBody.sphereOfInfluence)
{
errorMessage = "Warning: new Semi-Major Axis is very large, and may result in a hyberbolic orbit";
}
if (o.Radius(UT) > 2 * newSMA)
{
throw new OperationException("cannot make Semi-Major Axis less than twice the burn altitude plus the radius of " + o.referenceBody.theName + "(" + MuUtils.ToSI(o.referenceBody.Radius, 3) + "m)");
}
return(new ManeuverParameters(OrbitalManeuverCalculator.DeltaVForSemiMajorAxis(o, UT, newSMA), UT));
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
if (!target.NormalTargetExists)
{
throw new OperationException("must select a target to intercept.");
}
if (o.referenceBody != target.TargetOrbit.referenceBody)
{
throw new OperationException("target must be in the same sphere of influence.");
}
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
var dV = OrbitalManeuverCalculator.DeltaVToInterceptAtTime(o, UT, target.TargetOrbit, UT + interceptInterval);
return(new ManeuverParameters(dV, UT));
}
public override void DoParametersGUI(Orbit o, double universalTime, MechJebModuleTargetController target)
{
GuiUtils.SimpleTextBox("Time after burn to intercept target:", interceptInterval);
timeSelector.DoChooseTimeGUI();
}
public override void DoParametersGUI(Orbit o, double universalTime, MechJebModuleTargetController target)
{
GuiUtils.SimpleTextBox("Time after burn to intercept target:", interceptInterval);
timeSelector.DoChooseTimeGUI();
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
if (!target.NormalTargetExists)
{
throw new OperationException("must select a target to match planes with.");
}
else if (o.referenceBody != target.TargetOrbit.referenceBody)
{
throw new OperationException("can only match planes with an object in the same sphere of influence.");
}
else if (timeSelector.timeReference == TimeReference.REL_ASCENDING)
{
if (!o.AscendingNodeExists(target.TargetOrbit))
{
throw new OperationException("ascending node with target doesn't exist.");
}
}
else
{
if (!o.DescendingNodeExists(target.TargetOrbit))
{
throw new OperationException("descending node with target doesn't exist.");
}
}
Vector3d dV = (timeSelector.timeReference == TimeReference.REL_ASCENDING) ?
OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesAscending(o, target.TargetOrbit, UT, out UT):
OrbitalManeuverCalculator.DeltaVAndTimeToMatchPlanesDescending(o, target.TargetOrbit, UT, out UT);
return(new ManeuverParameters(dV, UT));
}
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("new apoapsis cannot be lower than the altitude of the burn (" + burnAltitude + ")");
}
return(new ManeuverParameters(OrbitalManeuverCalculator.DeltaVToChangeApoapsis(o, UT, newApA + o.referenceBody.Radius), UT));
}
public override void DoParametersGUI(Orbit o, double universalTime, MechJebModuleTargetController target)
{
GuiUtils.SimpleTextBox("New Semi-Major Axis:", newSMA, "km");
timeSelector.DoChooseTimeGUI();
}
public override void DoParametersGUI(Orbit o, double universalTime, MechJebModuleTargetController target)
{
GuiUtils.SimpleTextBox("New inclination:", newInc, "º");
timeSelector.DoChooseTimeGUI();
}
public override void DoParametersGUI(Orbit o, double universalTime, MechJebModuleTargetController target)
{
GuiUtils.SimpleTextBox("New periapsis:", newPeA, "km");
timeSelector.DoChooseTimeGUI();
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
return(new ManeuverParameters(OrbitalManeuverCalculator.DeltaVToCircularize(o, UT), UT));
}
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("new periapsis cannot be higher than the altitude of the burn (" + burnAltitude + ")");
}
else if (o.referenceBody.Radius + newApA < o.Radius(UT))
{
throw new OperationException("new apoapsis cannot be lower than the altitude of the burn (" + burnAltitude + ")");
}
else if (newPeA < -o.referenceBody.Radius)
{
throw new OperationException("new periapsis cannot be lower than minus the radius of " + o.referenceBody.displayName + "(-" + MuUtils.ToSI(o.referenceBody.Radius, 3) + "m)");
}
return(new ManeuverParameters(OrbitalManeuverCalculator.DeltaVToEllipticize(o, UT, newPeA + o.referenceBody.Radius, newApA + o.referenceBody.Radius), UT));
}
public override void DoParametersGUI(Orbit o, double universalTime, MechJebModuleTargetController target)
{
timeSelector.DoChooseTimeGUI();
}
