public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
var dV = OrbitalManeuverCalculator.DeltaVToShiftNodeLongitude(o, UT, target.targetLongitude);
return(new ManeuverParameters(dV, UT));
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
if (!target.NormalTargetExists)
{
throw new Exception("must select a target to match planes with.");
}
else if (o.referenceBody != target.TargetOrbit.referenceBody)
{
throw new Exception("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 Exception("ascending node with target doesn't exist.");
}
}
else
{
if (!o.DescendingNodeExists(target.TargetOrbit))
{
throw new Exception("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);
var dV = OrbitalManeuverCalculator.DeltaVToResonantOrbit(o, UT, (double)resonanceNumerator.val / resonanceDenominator.val);
return(new ManeuverParameters(dV, UT));
}
public override List <ManeuverParameters> MakeNodesImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
List <ManeuverParameters> NodeList = new List <ManeuverParameters>();
NodeList.Add(new ManeuverParameters(OrbitalManeuverCalculator.DeltaVToCircularize(o, UT), UT));
return(NodeList);
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
if (o.inclination < 10)
{
errorMessage = Localizer.Format("#MechJeb_AN_error", o.inclination);//"Warning: orbital plane has a low inclination of <<1>>º (recommend > 10º) and so maneuver may not be accurate"
}
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
var dV = OrbitalManeuverCalculator.DeltaVToShiftLAN(o, UT, target.targetLongitude);
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(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 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 = 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
}
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(Localizer.Format("#MechJeb_match_v_Exception1"));//must select a target to match velocities with.
}
else if (o.referenceBody != target.TargetOrbit.referenceBody)
{
throw new OperationException(Localizer.Format("#MechJeb_match_v_Exception2"));//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 (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));
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
if (!target.NormalTargetExists)
{
throw new Exception("must select a target to intercept.");
}
if (o.referenceBody != target.TargetOrbit.referenceBody)
{
throw new Exception("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 List <ManeuverParameters> MakeNodesImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
if (!target.NormalTargetExists)
{
throw new OperationException(Localizer.Format("#MechJeb_intercept_Exception1"));//must select a target to intercept.
}
if (o.referenceBody != target.TargetOrbit.referenceBody)
{
throw new OperationException(Localizer.Format("#MechJeb_intercept_Exception2"));//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);
List <ManeuverParameters> NodeList = new List <ManeuverParameters>();
NodeList.Add(new ManeuverParameters(dV, UT));
return(NodeList);
}
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));
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = 0;
if (!target.NormalTargetExists)
{
throw new OperationException("must select a target for the bi-impulsive transfer.");
}
else if (o.referenceBody != target.TargetOrbit.referenceBody)
{
throw new OperationException("target for bi-impulsive transfer must be in the same sphere of influence.");
}
var anExists = o.AscendingNodeExists(target.TargetOrbit);
var dnExists = o.DescendingNodeExists(target.TargetOrbit);
double anTime = o.TimeOfAscendingNode(target.TargetOrbit, universalTime);
double dnTime = o.TimeOfDescendingNode(target.TargetOrbit, universalTime);
if (timeSelector.timeReference == TimeReference.REL_ASCENDING)
{
if (!anExists)
{
throw new OperationException("ascending node with target doesn't exist.");
}
UT = anTime;
}
else if (timeSelector.timeReference == TimeReference.REL_DESCENDING)
{
if (!dnExists)
{
throw new OperationException("descending node with target doesn't exist.");
}
UT = dnTime;
}
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;
}
else
{
UT = dnTime;
}
}
else if (timeSelector.timeReference != TimeReference.COMPUTED)
{
UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
}
Vector3d dV;
if (timeSelector.timeReference == TimeReference.COMPUTED)
{
dV = OrbitalManeuverCalculator.DeltaVAndTimeForBiImpulsiveAnnealed(o, target.TargetOrbit, universalTime, out UT, intercept_only: intercept_only);
}
else
{
dV = OrbitalManeuverCalculator.DeltaVAndTimeForBiImpulsiveAnnealed(o, target.TargetOrbit, UT, out UT, intercept_only: intercept_only, fixed_ut: true);
}
return(new ManeuverParameters(dV, 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 ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
if (!target.NormalTargetExists)
{
throw new OperationException(Localizer.Format("#MechJeb_match_planes_Exception1"));//must select a target to match planes with.
}
else if (o.referenceBody != target.TargetOrbit.referenceBody)
{
throw new OperationException(Localizer.Format("#MechJeb_match_planes_Exception2"));//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(Localizer.Format("#MechJeb_match_planes_Exception3"));//ascending node with target doesn't exist.
}
UT = anTime;
dV = anDeltaV;
}
else if (timeSelector.timeReference == TimeReference.REL_DESCENDING)
{
if (!dnExists)
{
throw new OperationException(Localizer.Format("#MechJeb_match_planes_Exception4"));//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(Localizer.Format("#MechJeb_match_planes_Exception5"));//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(Localizer.Format("#MechJeb_match_planes_Exception5"));//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(Localizer.Format("#MechJeb_match_planes_Exception6"));//wrong time reference.
}
return(new ManeuverParameters(dV, UT));
}
public override ManeuverParameters MakeNodeImpl(Orbit o, double universalTime, MechJebModuleTargetController target)
{
double UT = 0;
if (!target.NormalTargetExists)
{
throw new OperationException(Localizer.Format("#MechJeb_Hohm_Exception1"));//must select a target for the bi-impulsive transfer.
}
else if (o.referenceBody != target.TargetOrbit.referenceBody)
{
throw new OperationException(Localizer.Format("#MechJeb_Hohm_Exception2"));//target for bi-impulsive transfer must be in the same sphere of influence.
}
Vector3d dV;
Orbit targetOrbit = target.TargetOrbit;
if (periodOffset != 0)
{
targetOrbit = target.TargetOrbit.Clone();
targetOrbit.MutatedOrbit(periodOffset: periodOffset);
}
if (simpleTransfer)
{
dV = OrbitalManeuverCalculator.DeltaVAndTimeForHohmannTransfer(o, targetOrbit, universalTime, out UT);
}
else
{
if (timeSelector.timeReference == TimeReference.COMPUTED)
{
dV = OrbitalManeuverCalculator.DeltaVAndTimeForBiImpulsiveAnnealed(o, targetOrbit, universalTime, out UT, intercept_only: intercept_only);
}
else
{
var anExists = o.AscendingNodeExists(target.TargetOrbit);
var dnExists = o.DescendingNodeExists(target.TargetOrbit);
double anTime = o.TimeOfAscendingNode(target.TargetOrbit, universalTime);
double dnTime = o.TimeOfDescendingNode(target.TargetOrbit, universalTime);
if (timeSelector.timeReference == TimeReference.REL_ASCENDING)
{
if (!anExists)
{
throw new OperationException(Localizer.Format("#MechJeb_Hohm_Exception3"));//ascending node with target doesn't exist.
}
UT = anTime;
}
else if (timeSelector.timeReference == TimeReference.REL_DESCENDING)
{
if (!dnExists)
{
throw new OperationException(Localizer.Format("#MechJeb_Hohm_Exception4"));//descending node with target doesn't exist.
}
UT = dnTime;
}
else if (timeSelector.timeReference == TimeReference.REL_NEAREST_AD)
{
if (!anExists && !dnExists)
{
throw new OperationException(Localizer.Format("#MechJeb_Hohm_Exception5"));//neither ascending nor descending node with target exists.
}
if (!dnExists || anTime <= dnTime)
{
UT = anTime;
}
else
{
UT = dnTime;
}
}
UT = timeSelector.ComputeManeuverTime(o, universalTime, target);
dV = OrbitalManeuverCalculator.DeltaVAndTimeForBiImpulsiveAnnealed(o, targetOrbit, UT, out UT, intercept_only: intercept_only, fixed_ut: true);
}
}
return(new ManeuverParameters(dV, UT));
}
