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Kerbal Space Program
1.12.4
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Kerbal Space Program
1.12.4
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This is the complete list of members for TransferMath, including all inherited members.
| AlignmentTime(TransferDataSimple transferDataSimple, Orbit sourceOrbit, Orbit targetOrbit, double startUT, double offsetDegrees=0d) | TransferMath | inlinestatic |
| Bisect(BisectFunc f, double minimum, double maximum, double acceptableRange=0.01, int maxIter=15) | TransferMath | inlinestatic |
| BisectFunc(double x) | TransferMath | |
| CalcCircularizeDV(TransferDataSimple transferDataSimple, double newApoapsis) | TransferMath | inlinestatic |
| CalcSameSOITransferDV(TransferDataSimple transferDataSimple, Orbit startOrbit) | TransferMath | inlinestatic |
| CalculateCorrection(TransferDataSimple transferDataSimple, double startUT, SafeAbortBackgroundWorker bw) | TransferMath | inlinestatic |
| CalculateStartEndXferTimes(CelestialBody sourceBody, CelestialBody targetBody, double offsetDegrees, out double startTime, out double endTime) | TransferMath | inlinestatic |
| CalculateStartEndXferTimes(CelestialBody sourceBody, CelestialBody targetBody, double afterUT, double offsetDegrees, out double startTime, out double endTime) | TransferMath | inlinestatic |
| CalculateStartEndXferTimes(TransferDataSimple transferDataSimple, CelestialBody sourceBody, CelestialBody targetBody, double offsetDegrees, out string startTime, out string endTime) | TransferMath | inlinestatic |
| ChangingPeriapsis(Orbit start, Orbit target, double UT) | TransferMath | inlinestatic |
| DeltaVToInterceptAtTime(Orbit o, double initialUT, Orbit target, double DT, out Vector3d secondDV) | TransferMath | inlinestatic |
| FinalizeLambert(TransferDataSimple transferDataSimple, double startUT, Orbit startOrbit, Orbit targetOrbit) | TransferMath | inlinestatic |
| FindIntercept(TransferDataSimple transferDataSimple, Orbit startOrbit, CelestialBody targetBody, Vector3d dV, double UT, bool sameSOIXfer, double initialClosestApproach, SafeAbortBackgroundWorker bw, out Vector3d adjustedDV) | TransferMath | inlinestatic |
| HohmannTimeOfFlight(Orbit origin, Orbit destination) | TransferMath | inlinestatic |
| LambertSolver(double mu, Vector3d r1, Vector3d v1, Vector3d r2, Vector3d v2, double tof, int nrev, out Vector3d vi, out Vector3d vf) | TransferMath | inlinestatic |
| Root(BisectFunc f, double a, double b, double tol, int maxIterations=50, int sign=0) | TransferMath | inlinestatic |
| SafeOrbitRadius(CelestialBody body) | TransferMath | inlinestatic |
| safetyEnvelope | TransferMath | static |
| SameSOITransfer(TransferDataSimple transferDataSimple) | TransferMath | inlinestatic |
| SuperiorLambert(double mu, Vector3d r1, Vector3d v1, Vector3d r2, Vector3d v2, double tof, out Vector3d vi, out Vector3d vf) | TransferMath | inlinestatic |
| TransferDV(TransferDataSimple transferDataSimple, double startUT) | TransferMath | inlinestatic |
1.8.7