This is the complete list of members for GravityEngine2.Orbital, including all inherited members.

CheckHitPlanet(double planetRadius, double planetMass, double3 r1c, double3 v1tc, double3 r2c, double3 v2tc, int nrev) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
COEEqual(COE coe1, COE coe2, bool includePhase, double sizeTol=1E-2, double angleRadTol=1E-3)	GravityEngine2.Orbital	static
COEStructWithPhasetoRVRelative(COEStruct coe, double phaseRad) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
COEtoRVatTime(COE coe, double time) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
COEtoRVRelative(COE oe) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
COEWithPhasetoRVRelative(COE oe, double phaseRad) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
ConvertBToTrueAnomoly(double B, double p, double r) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
ConvertEtoMeanAnomoly(double eValue, double ecc) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
ConvertEtoTrueAnomoly(double eValue, double ecc)	GravityEngine2.Orbital	static
ConvertHToTrueAnomoly(double H, double e) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
ConvertMeanAnomolyToE(double M, double ecc) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
ConvertMeanToTrueAnomoly(double M, double ecc) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
ConvertTrueAnomolytoE(double nu, double ecc) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
double3	GravityEngine2.Orbital	static
FindC2C3(double znew, out double c2new, out double c3new)	GravityEngine2.Orbital	static
FlightPathAngle(double3 r, double3 v) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
GreenwichSiderealTime(double jdate)	GravityEngine2.Orbital	static
KeplerEqnHyperbolicForH(double M, double e) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
KeplerEqnParabolicForB(double dt, double p, double mu) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
LaunchPlane(double targetInclDeg, double3 r, double latitudeDeg)	GravityEngine2.Orbital	static
M (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
NewtonNu(double ecc, double nu, double small) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
OrbitAxis(COE coe)	GravityEngine2.Orbital	static
OrbitPoint enum name (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital
OrbitType enum name (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital
PhaseAngleRadiansForDirection(double3 pos, COE coe)	GravityEngine2.Orbital	static
PhaseForOrbitPoint(COE coe, OrbitPoint point, double deg=0)	GravityEngine2.Orbital	static
PhaseForRadius(COE coe, double radius)	GravityEngine2.Orbital	static
PositionForCOE(COE coe, double phaseRad)	GravityEngine2.Orbital	static
PositionsForR(COE coe, double r) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
r	GravityEngine2.Orbital	static
RotateToOrbitFrame(COE coe, double3 r)	GravityEngine2.Orbital	static
RSWState(ref GEBodyState ship, ref GEBodyState planet, double3 orbitNormal, ref GEBodyState rswState)	GravityEngine2.Orbital	static
RVForOrbitPoint(COE coe, OrbitPoint point, double deg=0) (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
RVtoCOE(double3 r, double3 v, double mu, double small=1e-6)	GravityEngine2.Orbital	static
SMALL_ANGLE (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
SMALL_E (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
SMALL_P (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
SMALL_SME (defined in GravityEngine2.Orbital)	GravityEngine2.Orbital	static
SoiRadius(double planetMass, double moonMass, double moonSemiMajorAxis)	GravityEngine2.Orbital	static
TimeOfFlight(double3 r0, double3 r1, COE coe)	GravityEngine2.Orbital	static
VDirFromFPAandRR(double fpa, double3 r1, double3 r2)	GravityEngine2.Orbital	static
VelocityForCircularOrbitRelative(GEBodyState body, double mu)	GravityEngine2.Orbital	static
VelocityForCOE(COE coe, double phaseRad)	GravityEngine2.Orbital	static
VelocityIsPrograde(double3 r, double3 v_now, double3 v_next)	GravityEngine2.Orbital	static
VelocityMagnitudeForCircular(double r, double mu)	GravityEngine2.Orbital	static