Table of Contents

Class PatchedNBodyOrbit

Namespace
KSP.Sim.impl
Assembly
Assembly-CSharp.dll
public class PatchedNBodyOrbit : IPatchedOrbit, IDisposable, IComparable<IPatchedOrbit>, IDynamicOrbit, IOrbit
Inheritance
PatchedNBodyOrbit
Implements
Inherited Members
Extension Methods

Constructors

PatchedNBodyOrbit() 

public PatchedNBodyOrbit()

Fields

AArray 

public NativeArray<double> AArray

Field Value

NativeArray<double>

BArray 

public NativeArray<double> BArray

Field Value

NativeArray<double>

BURST_ALLOCATOR_TYPE 

public const Allocator BURST_ALLOCATOR_TYPE = 4

Field Value

Allocator

CArray 

public NativeArray<double> CArray

Field Value

NativeArray<double>

EArray 

public NativeArray<double> EArray

Field Value

NativeArray<double>

EncounterBodyIndex 

public NativeArray<int> EncounterBodyIndex

Field Value

NativeArray<int>

ErrorEstimateOrder 

public int ErrorEstimateOrder

Field Value

int

KArray 

public NativeArray<PatchedNBody.OdeState> KArray

Field Value

NativeArray<OdeState>

MAX_ITERATIONS 

public const int MAX_ITERATIONS = 50

Field Value

int

OdeChildKeplerBodies 

public NativeList<PatchedNBody.CelestialBodyPositionJob.KeplerBody> OdeChildKeplerBodies

Field Value

NativeList<KeplerBody>

OdeSolveJob 

public PatchedNBody.OdeSolveJob OdeSolveJob

Field Value

PatchedNBody.OdeSolveJob

OdeSolveTerminationStatus 

public NativeArray<OdeSolveStatus> OdeSolveTerminationStatus

Field Value

NativeArray<OdeSolveStatus>

PArray 

public NativeArray<double> PArray

Field Value

NativeArray<double>

PShape 

public int2 PShape

Field Value

int2

PatchEndTransitionNative 

public NativeArray<PatchTransitionType> PatchEndTransitionNative

Field Value

NativeArray<PatchTransitionType>

QArray 

public NativeList<PatchedNBody.OdeState> QArray

Field Value

NativeList<OdeState>

TOLERANCE 

public const double TOLERANCE = 0.01

Field Value

double

Properties

ActivePatch 

public bool ActivePatch { get; set; }

Property Value

bool

Apoapsis 

public double Apoapsis { get; }

Property Value

double

ApoapsisArl 

public double ApoapsisArl { get; }

Property Value

double

ClosestApproachDistance 

public double ClosestApproachDistance { get; set; }

Property Value

double

EndUT 

public double EndUT { get; set; }

Property Value

double

NextPatch 

public IPatchedOrbit NextPatch { get; set; }

Property Value

IPatchedOrbit

OdeSolution 

public NativeList<PatchedNBody.OdeSolutionComponent> OdeSolution { get; }

Property Value

NativeList<OdeSolutionComponent>

OrbitFrame 

public CelestialFrame OrbitFrame { get; }

Property Value

CelestialFrame

OrbitMarkerHandler 

public OrbitMarkerHandler OrbitMarkerHandler { get; }

Property Value

OrbitMarkerHandler

PatchEndTransition 

public PatchTransitionType PatchEndTransition { get; set; }

Property Value

PatchTransitionType

PatchStartTransition 

public PatchTransitionType PatchStartTransition { get; set; }

Property Value

PatchTransitionType

Periapsis 

public double Periapsis { get; }

Property Value

double

PeriapsisArl 

public double PeriapsisArl { get; }

Property Value

double

Position 

public Position Position { get; }

Property Value

Position

PreviousPatch 

public IPatchedOrbit PreviousPatch { get; set; }

Property Value

IPatchedOrbit

ReferenceFrame 

public ITransformFrame ReferenceFrame { get; }

Property Value

ITransformFrame

SolverParams 

public PatchedNBodyOrbit.SolverParameters SolverParams { get; }

Property Value

PatchedNBodyOrbit.SolverParameters

SpecificAngularMomentum 

public Vector3d SpecificAngularMomentum { get; }

Property Value

Vector3d

StartUT 

public double StartUT { get; set; }

Property Value

double

TimeToAp 

public double TimeToAp { get; set; }

Property Value

double

TimeToPe 

public double TimeToPe { get; set; }

Property Value

double

UniversalTimeAtClosestApproach 

public double UniversalTimeAtClosestApproach { get; set; }

Property Value

double

UniversalTimeAtSoiEncounter 

public double UniversalTimeAtSoiEncounter { get; set; }

Property Value

double

coordinateSystem 

public ICoordinateSystem coordinateSystem { get; }

Property Value

ICoordinateSystem

localPosition 

public Vector3d localPosition { get; }

Property Value

Vector3d

referenceBody 

public CelestialBodyComponent referenceBody { get; }

Property Value

CelestialBodyComponent

relativeToMotion 

public IMotion relativeToMotion { get; }

Property Value

IMotion

relativeVelocity 

public Vector relativeVelocity { get; }

Property Value

Vector

Methods

CompareTo(IPatchedOrbit) 

public int CompareTo(IPatchedOrbit other)

Parameters

other IPatchedOrbit

Returns

int

CreateInterpolator() 

public void CreateInterpolator()

Dispose() 

public void Dispose()

DisposeMarkerHandler() 

public void DisposeMarkerHandler()

GetOrbitalStateVectorsAtUT(double, out Vector3d, out Vector3d) 

public double GetOrbitalStateVectorsAtUT(double UT, out Vector3d localPositionZup, out Vector3d relativeVelocityZup)

Parameters

UT double
localPositionZup Vector3d
relativeVelocityZup Vector3d

Returns

double

GetOrbitalVelocityAtUTZup(double) 

public Vector3d GetOrbitalVelocityAtUTZup(double UT)

Parameters

UT double

Returns

Vector3d

GetRelativePositionAtUT(double) 

public Vector3d GetRelativePositionAtUT(double UT)

Parameters

UT double

Returns

Vector3d

GetRelativePositionAtUTZup(double) 

public Vector3d GetRelativePositionAtUTZup(double UT)

Parameters

UT double

Returns

Vector3d

GetRelativePositionFromEccAnomaly(double) 

public Vector3d GetRelativePositionFromEccAnomaly(double eccentricAnomaly)

Parameters

eccentricAnomaly double

Returns

Vector3d

GetRelativeVelocityAtUT(double) 

public Vector3d GetRelativeVelocityAtUT(double UT)

Parameters

UT double

Returns

Vector3d

GetTimeToPeriapsis() 

public double GetTimeToPeriapsis()

Returns

double

GetTruePositionAtT(double) 

public Position GetTruePositionAtT(double universalTime)

Parameters

universalTime double

Returns

Position

GetTruePositionAtT(double, ICoordinateSystem) 

public Vector3d GetTruePositionAtT(double universalTime, ICoordinateSystem coordinateSystem)

Parameters

universalTime double
coordinateSystem ICoordinateSystem

Returns

Vector3d

GetTruePositionAtUT(double) 

public Position GetTruePositionAtUT(double universalTime)

Parameters

universalTime double

Returns

Position

GetTruePositionAtUT(double, ICoordinateSystem) 

public Vector3d GetTruePositionAtUT(double universalTime, ICoordinateSystem coordinateSystem)

Parameters

universalTime double
coordinateSystem ICoordinateSystem

Returns

Vector3d

GetVel(VesselComponent) 

public Vector3d GetVel(VesselComponent relativeVessel)

Parameters

relativeVessel VesselComponent

Returns

Vector3d

InitializeMarkerHandler() 

public void InitializeMarkerHandler()

InitializeOdeSolverData() 

public void InitializeOdeSolverData()

OnOdeSolveComplete(PatchTransitionType) 

public void OnOdeSolveComplete(PatchTransitionType patchEndTransitionType)

Parameters

patchEndTransitionType PatchTransitionType

SetReferenceBody(CelestialBodyComponent) 

public void SetReferenceBody(CelestialBodyComponent body)

Parameters

body CelestialBodyComponent

SetSolverParams(double, double, double3, double3, CelestialBodyComponent) 

public void SetSolverParams(double startUt, double endUt, double3 initialPosition, double3 initialVelocity, CelestialBodyComponent parentBody)

Parameters

startUt double
endUt double
initialPosition double3
initialVelocity double3
parentBody CelestialBodyComponent

SolveClosestApproach(IKeplerOrbit, ref double, double, double, double, double, int, ref int) 

public double SolveClosestApproach(IKeplerOrbit secondaryKeplerOrbit, ref double UT, double dT, double minUt, double maxUt, double epsilon, int maxIterations, ref int iterationCount)

Parameters

secondaryKeplerOrbit IKeplerOrbit
UT double
dT double
minUt double
maxUt double
epsilon double
maxIterations int
iterationCount int

Returns

double

SolveSOI_BSP(IKeplerOrbit, ref double, double, double, double, double, double, int, ref int) 

public bool SolveSOI_BSP(IKeplerOrbit secondaryKeplerOrbit, ref double UT, double dT, double Rsoi, double MinUT, double MaxUT, double epsilon, int maxIterations, ref int iterationCount)

Parameters

secondaryKeplerOrbit IKeplerOrbit
UT double
dT double
Rsoi double
MinUT double
MaxUT double
epsilon double
maxIterations int
iterationCount int

Returns

bool

UpdateFromOrbitAtUT(IOrbit, double, CelestialBodyComponent) 

public void UpdateFromOrbitAtUT(IOrbit orbit, double UT, CelestialBodyComponent toBody)

Parameters

orbit IOrbit
UT double
toBody CelestialBodyComponent

UpdateFromStateVectors(ICoordinateSystem, Vector3d, IMotion, Vector3d, CelestialBodyComponent, double) 

public void UpdateFromStateVectors(ICoordinateSystem coordinateSystem, Vector3d pos, IMotion relativeMotion, Vector3d vel, CelestialBodyComponent refBody, double UT)

Parameters

coordinateSystem ICoordinateSystem
pos Vector3d
relativeMotion IMotion
vel Vector3d
refBody CelestialBodyComponent
UT double

UpdateFromStateVectors(Position, Velocity, CelestialBodyComponent, double) 

public void UpdateFromStateVectors(Position pos, Velocity vel, CelestialBodyComponent refBody, double UT)

Parameters

pos Position
vel Velocity
refBody CelestialBodyComponent
UT double

UpdateFromUT(double) 

public void UpdateFromUT(double UT)

Parameters

UT double