Gravity Engine 12.0
Unity Asset for Gravity
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This is the complete list of members for OrbitUtils, including all inherited members.
CalcAForPeriod(double period, double centerMass) | OrbitUtils | static |
CalcKeplerDepth(IFixedOrbit fixedBody) | OrbitUtils | static |
CenterOfMass(NBody body1, NBody body2) (defined in OrbitUtils) | OrbitUtils | static |
CheckHitPlanet(double planetRadius, double planetMass, Vector3d r1c, Vector3d v1tc, Vector3d r2c, Vector3d v2tc, int nrev) (defined in OrbitUtils) | OrbitUtils | static |
COEtoRV(OrbitElements oe, NBody centerBody, ref Vector3d r, ref Vector3d v, bool relativePos) (defined in OrbitUtils) | OrbitUtils | static |
COEtoRV(OrbitElements oe, NBody centerBody, double mu, ref Vector3d r, ref Vector3d v, bool relativePos, double ecc_threshold=small, double incl_threshold=small) (defined in OrbitUtils) | OrbitUtils | static |
COEtoRVMirror(OrbitElements oe, NBody centerBody, ref Vector3d r, ref Vector3d v, bool relativePos) (defined in OrbitUtils) | OrbitUtils | static |
COEtoRVRelative(OrbitElements oe, double mu, ref Vector3d r, ref Vector3d v) (defined in OrbitUtils) | OrbitUtils | static |
ConvertEtoMeanAnomoly(double eValue, double ecc) (defined in OrbitUtils) | OrbitUtils | static |
ConvertEtoTrueAnomoly(double eValue, double ecc) | OrbitUtils | static |
ConvertMeanAnomolyToE(double M, double ecc) (defined in OrbitUtils) | OrbitUtils | static |
ConvertTrueAnomolytoE(double nu, double ecc) (defined in OrbitUtils) | OrbitUtils | static |
ecc_circular (defined in OrbitUtils) | OrbitUtils | static |
FindC2C3(double znew, out double c2new, out double c3new) (defined in OrbitUtils) | OrbitUtils | static |
FindNodes(OrbitPredictor ship, OrbitPredictor target) (defined in OrbitUtils) | OrbitUtils | static |
FlightPathAngle(double sin_nu, double cos_nu, double ecc) | OrbitUtils | static |
GetCenterNbody(Transform objectInOrbit, GameObject centerObject) | OrbitUtils | static |
GetPhaseFromOE(OrbitUtils.OrbitElements oe, double ecc_threshold=small, double incl_threshold=small) | OrbitUtils | static |
GsTime(double jdut1) (defined in OrbitUtils) | OrbitUtils | static |
HillRadius(GameObject primary, GameObject secondary) | OrbitUtils | static |
IsOnRails(NBody nbody) (defined in OrbitUtils) | OrbitUtils | static |
LsTime(double lon, double jdut1, out double lst, out double gst) (defined in OrbitUtils) | OrbitUtils | static |
PhaseAngleRadiansForDirection(Vector3d pos, OrbitElements oe) (defined in OrbitUtils) | OrbitUtils | static |
RVtoCOE(Vector3 r_in, Vector3 v_in, NBody centerBody, float mu, bool relativePos, double ecc_threshold=small, double incl_threshold=small) (defined in OrbitUtils) | OrbitUtils | static |
RVtoCOE(Vector3 r_in, Vector3 v_in, NBody centerBody, bool relativePos, double ecc_threshold=small, double incl_threshold=small) (defined in OrbitUtils) | OrbitUtils | static |
RVtoCOE(Vector3d r_in, Vector3d v_in, NBody centerBody, bool relativePos, double ecc_threshold=small, double incl_threshold=small) | OrbitUtils | static |
RVtoCOE(Vector3d r_in, Vector3d v_in, NBody centerBody, double mu, bool relativePos, double ecc_threshold=small, double incl_threshold=small) (defined in OrbitUtils) | OrbitUtils | static |
small (defined in OrbitUtils) | OrbitUtils | static |
SoiRadius(NBody planet, NBody moon) | OrbitUtils | static |
TimeOfFlight(Vector3d r0, Vector3d r1, double p, double mu, Vector3d normal) | OrbitUtils | static |
TimeOfFlightEllipse(Vector3d r0, Vector3d r1, Vector3d axis, double eccentricity, double orbit_period) | OrbitUtils | static |
TransformToOrbitFrame(Vector3d v, OrbitElements oe) | OrbitUtils | static |
Vector3 (defined in OrbitUtils) | OrbitUtils | static |
verySmall (defined in OrbitUtils) | OrbitUtils | static |