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Kerbal Space Program
1.12.4
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All Classes Namespaces Files Functions Variables Typedefs Enumerations Enumerator Properties Events Macros
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Kerbal Space Program
1.12.4
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This is the complete list of members for Orbit, including all inherited members.
| _FindClosestPoints(Orbit p, Orbit s, ref double CD, ref double CCD, ref double FFp, ref double FFs, ref double SFp, ref double SFs, double epsilon, int maxIterations, ref int iterationCount) | Orbit | inlinestatic |
| _SolveClosestApproach(Orbit p, Orbit s, ref double UT, double dT, double threshold, double MinUT, double MaxUT, double epsilon, int maxIterations, ref int iterationCount) | Orbit | inlinestatic |
| _SolveSOI(Orbit p, Orbit s, ref double UT, double dT, double Rsoi, double MinUT, double MaxUT, double epsilon, int maxIterations, ref int iterationCount) | Orbit | inlinestatic |
| _SolveSOI_BSP(Orbit p, Orbit s, ref double UT, double dT, double Rsoi, double MinUT, double MaxUT, double epsilon, int maxIterations, ref int iterationCount) | Orbit | inlinestatic |
| activePatch | Orbit | |
| altitude | Orbit | |
| ApA | Orbit | |
| ApR | Orbit | |
| argumentOfPeriapsis | Orbit | |
| AscendingNodeTrueAnomaly(Orbit p, Orbit s) | Orbit | inlinestatic |
| closestEncounterBody | Orbit | |
| closestEncounterLevel | Orbit | |
| closestEncounterPatch | Orbit | |
| closestTgtApprUT | Orbit | |
| CreateRandomOrbitAround(CelestialBody body) | Orbit | inlinestatic |
| CreateRandomOrbitAround(CelestialBody body, double minAltitude, double maxAltitude) | Orbit | inlinestatic |
| CreateRandomOrbitFlyBy(CelestialBody tgtBody, double daysToClosestApproach) | Orbit | inlinestatic |
| CreateRandomOrbitFlyBy(Orbit targetOrbit, double timeToPeriapsis, double periapsis, double deltaVatPeriapsis) | Orbit | inlinestatic |
| CreateRandomOrbitNearby(Orbit baseOrbit) | Orbit | inlinestatic |
| debug_returnFullEllipseTrajectory | Orbit | |
| debugPos | Orbit | |
| Deg2Rad | Orbit | |
| DescendingNodeTrueAnomaly(Orbit p, Orbit s) | Orbit | inlinestatic |
| DrawOrbit() | Orbit | inline |
| DrawOrbit(Color color) | Orbit | inline |
| eccentricAnomaly | Orbit | |
| EccentricAnomalyAtObT(double T) | Orbit | inline |
| EccentricAnomalyAtUT(double UT) | Orbit | inline |
| eccentricity | Orbit | |
| EncounterSolutionLevel enum name | Orbit | |
| EndUT | Orbit | |
| epoch | Orbit | |
| FEVp | Orbit | |
| FindClosestPoints | Orbit | static |
| FindClosestPoints_old(Orbit p, Orbit s, ref double CD, ref double CCD, ref double FFp, ref double FFs, ref double SFp, ref double SFs, double epsilon, int maxIterations, ref int iterationCount) | Orbit | inlinestatic |
| FindClosestPointsDelegate(Orbit p, Orbit s, ref double CD, ref double CCD, ref double FFp, ref double FFs, ref double SFp, ref double SFs, double epsilon, int maxIterations, ref int iterationCount) | Orbit | |
| fromE | Orbit | |
| GetANVector() | Orbit | inline |
| GetDTforTrueAnomaly(double tA, double wrapAfterSeconds) | Orbit | inline |
| GetDTforTrueAnomalyAtUT(double tA, double UT) | Orbit | inline |
| GetEccentricAnomaly(double tA) | Orbit | inline |
| GetEccVector() | Orbit | inline |
| GetFrameVel() | Orbit | inline |
| GetFrameVelAtUT(double UT) | Orbit | inline |
| GetMeanAnomaly(double E) | Orbit | inline |
| getMeanAnomalyAtUT(double UT) | Orbit | inline |
| GetMeanMotion(double sma) | Orbit | inline |
| GetNextApoapsisTime(double UT) | Orbit | inline |
| GetNextPeriapsisTime(double UT) | Orbit | inline |
| GetNextTimeOfRadius(double UT, double radius) | Orbit | inline |
| getObTAtMeanAnomaly(double M) | Orbit | inline |
| getObtAtTrueAnomaly(double tA) | Orbit | inline |
| getObtAtUT(double UT) | Orbit | inline |
| GetOrbitalCurvatureAtTrueAnomaly(double ta) | Orbit | inline |
| getOrbitalSpeedAt(double time) | Orbit | inline |
| getOrbitalSpeedAtDistance(double d) | Orbit | inline |
| getOrbitalSpeedAtPos(Vector3d pos) | Orbit | inline |
| getOrbitalSpeedAtRelativePos(Vector3d relPos) | Orbit | inline |
| GetOrbitalStateVectorsAtObT(double ObT, double UT, out Vector3d pos, out Vector3d vel) | Orbit | inline |
| GetOrbitalStateVectorsAtObT(double ObT, out State state) | Orbit | inline |
| GetOrbitalStateVectorsAtTrueAnomaly(double tA, double UT, out Vector3d pos, out Vector3d vel) | Orbit | inline |
| GetOrbitalStateVectorsAtTrueAnomaly(double tA, double UT, bool worldToLocal, out Vector3d pos, out Vector3d vel) | Orbit | inline |
| GetOrbitalStateVectorsAtTrueAnomaly(double tA, out State state) | Orbit | inline |
| GetOrbitalStateVectorsAtUT(double UT, out Vector3d pos, out Vector3d vel) | Orbit | inline |
| GetOrbitalStateVectorsAtUT(double UT, out State state) | Orbit | inline |
| getOrbitalVelocityAtObT(double ObT) | Orbit | inline |
| getOrbitalVelocityAtTrueAnomaly(double tA) | Orbit | inline |
| getOrbitalVelocityAtTrueAnomaly(double tA, bool worldToLocal) | Orbit | inline |
| getOrbitalVelocityAtUT(double UT) | Orbit | inline |
| GetOrbitNormal() | Orbit | inline |
| getPositionAtT(double T) | Orbit | inline |
| getPositionAtUT(double UT) | Orbit | inline |
| getPositionFromEccAnomaly(double E) | Orbit | inline |
| getPositionFromEccAnomalyWithSemiMinorAxis(double E, double semiMinorAxis) | Orbit | inline |
| getPositionFromMeanAnomaly(double M) | Orbit | inline |
| getPositionFromTrueAnomaly(double tA) | Orbit | inline |
| getPositionFromTrueAnomaly(double tA, bool worldToLocal) | Orbit | inline |
| GetRadiusAtPhaseAngle(double phaseAngle) | Orbit | inline |
| GetRadiusAtUT(double time) | Orbit | inline |
| GetRelativeInclination(Orbit otherOrbit) | Orbit | inline |
| getRelativePositionAtT(double T) | Orbit | inline |
| getRelativePositionAtUT(double UT) | Orbit | inline |
| getRelativePositionFromEccAnomaly(double E) | Orbit | inline |
| getRelativePositionFromEccAnomalyWithSemiMinorAxis(double E, double semiMinorAxis) | Orbit | inline |
| getRelativePositionFromMeanAnomaly(double M) | Orbit | inline |
| getRelativePositionFromTrueAnomaly(double tA) | Orbit | inline |
| GetRelativeVel() | Orbit | inline |
| GetRotFrameVel(CelestialBody refBody) | Orbit | inline |
| GetRotFrameVelAtPos(CelestialBody refBody, Vector3d refPos) | Orbit | inline |
| GetTimeToPeriapsis() | Orbit | inline |
| GetTrueAnomaly(double E) | Orbit | inline |
| GetTrueAnomalyOfZupVector(Vector3d vector) | Orbit | inline |
| getTruePositionAtUT(double UT) | Orbit | inline |
| getUTAtMeanAnomaly(double M, double UT) | Orbit | inline |
| GetUTforTrueAnomaly(double tA, double wrapAfterSeconds) | Orbit | inline |
| GetVel() | Orbit | inline |
| GetWorldSpaceVel() | Orbit | inline |
| h | Orbit | |
| Horizontal(double UT) | Orbit | inline |
| inclination | Orbit | |
| Init() | Orbit | inline |
| LAN | Orbit | |
| mag | Orbit | |
| meanAnomaly | Orbit | |
| meanAnomalyAtEpoch | Orbit | |
| meanMotion | Orbit | |
| NextCloseApproachTime(Orbit p, Orbit s, double UT) | Orbit | inlinestatic |
| nextPatch | Orbit | |
| Normal(double UT) | Orbit | inline |
| numClosePoints | Orbit | |
| ObjectType enum name | Orbit | |
| objectType | Orbit | |
| ObT | Orbit | |
| ObTAtEpoch | Orbit | |
| Orbit() | Orbit | inline |
| Orbit(double inc, double e, double sma, double lan, double argPe, double mEp, double t, CelestialBody body) | Orbit | inline |
| Orbit(Orbit orbit) | Orbit | inline |
| orbitalEnergy | Orbit | |
| orbitalSpeed | Orbit | |
| OrbitFrame | Orbit | |
| OrbitFrameX | Orbit | |
| OrbitFromStateVectors(Vector3d pos, Vector3d vel, CelestialBody body, double UT) | Orbit | inlinestatic |
| orbitPercent | Orbit | |
| patchEndTransition | Orbit | |
| patchStartTransition | Orbit | |
| PatchTransitionType enum name | Orbit | |
| PeA | Orbit | |
| PeApIntersects(Orbit primary, Orbit secondary, double threshold) | Orbit | inlinestatic |
| PeR | Orbit | |
| period | Orbit | |
| PhaseAngle(double time, double longitude) | Orbit | inline |
| PhaseAngle(double time) | Orbit | inline |
| pos | Orbit | |
| Prograde(double UT) | Orbit | inline |
| Rad2Deg | Orbit | |
| Radial(double UT) | Orbit | inline |
| radius | Orbit | |
| RadiusAtTrueAnomaly(double tA) | Orbit | inline |
| referenceBody | Orbit | |
| RelativeInclination(Orbit p, Orbit s) | Orbit | inlinestatic |
| RelativeStateAtUT(Orbit p, Orbit s, double UT, out State pstate, out State sstate, out State rstate, bool dump=false) | Orbit | inlinestatic |
| SafeAcos(double c) | Orbit | inlinestatic |
| secondaryPosAtTransition1 | Orbit | |
| semiLatusRectum | Orbit | |
| semiMajorAxis | Orbit | |
| semiMinorAxis | Orbit | |
| SetOrbit(double inc, double e, double sma, double lan, double argPe, double mEp, double t, CelestialBody body) | Orbit | inline |
| SolveClosestApproach | Orbit | static |
| SolveClosestApproachDelegate(Orbit p, Orbit s, ref double UT, double dT, double threshold, double MinUT, double MaxUT, double epsilon, int maxIterations, ref int iterationCount) | Orbit | |
| solveEccentricAnomaly(double M, double ecc, double maxError=1e-7, int maxIterations=8) | Orbit | inline |
| SolveSOI | Orbit | static |
| SolveSOI_BSP | Orbit | static |
| SolveSOI_BSPDelegate(Orbit p, Orbit s, ref double UT, double dT, double Rsoi, double MinUT, double MaxUT, double epsilon, int maxIterations, ref int iterationCount) | Orbit | |
| SolveSOI_Delegate(Orbit p, Orbit s, ref double UT, double dT, double Rsoi, double MinUT, double MaxUT, double epsilon, int maxIterations, ref int iterationCount) | Orbit | |
| StartUT | Orbit | |
| Swizzle(Vector3d vec) | Orbit | inlinestatic |
| SynodicPeriod(Orbit o1, Orbit o2) | Orbit | inlinestatic |
| TimeOfTrueAnomaly(double tA, double UT) | Orbit | inline |
| timeToAp | Orbit | |
| timeToPe | Orbit | |
| timeToTransition1 | Orbit | |
| trueAnomaly | Orbit | |
| TrueAnomalyAtRadius(double R) | Orbit | inline |
| TrueAnomalyAtT(double T) | Orbit | inline |
| TrueAnomalyAtUT(double UT) | Orbit | inline |
| TrueAnomalyFromVector(Vector3d vec) | Orbit | inline |
| Up(double UT) | Orbit | inline |
| UpdateFromFixedVectors(Vector3d pos, Vector3d vel, CelestialBody refBody, double UT) | Orbit | inline |
| UpdateFromOrbitAtUT(Orbit orbit, double UT, CelestialBody toBody) | Orbit | inline |
| UpdateFromStateVectors(Vector3d pos, Vector3d vel, CelestialBody refBody, double UT) | Orbit | inline |
| UpdateFromUT(double UT) | Orbit | inline |
1.8.7