Inheritance diagram for GravityEngine2.OrbitDisplayCommon:

Static Public Member Functions
static void	OrbitPositions (Orbital.COE coe, ref Vector3[] points, bool snapToShip=true)
	Determine the orbit positions assuming center at (0,0,0). The scale is set by coe.p.

static Vector3[]	OrbitPositionsEllipseByE (Orbital.COE coe, int numPoints)
	Provide equally spaced point around the ellipse by iterating over the eccentric anamoly.

static Vector3[]	OrbitPositionsToFromTA (Orbital.COE coe, int numPoints, double fromTARad, double toTARad)
	Determine the orbit positions assuming center at (0,0,0). The scale is set by coe.p.

Member Function Documentation

◆ OrbitPositions()

static void GravityEngine2.OrbitDisplayCommon.OrbitPositions	(	Orbital::COE	coe,
		ref Vector3[]	points,
		bool	snapToShip = true )

static

Determine the orbit positions assuming center at (0,0,0). The scale is set by coe.p.

Parameters

static Vector3[] GravityEngine2.OrbitDisplayCommon.OrbitPositionsEllipseByE	(	Orbital::COE	coe,
		int	numPoints )

static

Provide equally spaced point around the ellipse by iterating over the eccentric anamoly.

REF: Idea from DiPrinzo "Methods of Orbital Maneuvering" AIAA Press.

Parameters

static Vector3[] GravityEngine2.OrbitDisplayCommon.OrbitPositionsToFromTA	(	Orbital::COE	coe,
		int	numPoints,
		double	fromTARad,
		double	toTARad )

static

Determine the orbit positions assuming center at (0,0,0). The scale is set by coe.p.

If the orbit is an ellipse then the points can wrap from the to to the from TA.

If the orbit is a hyperbola then a cutoff is applied to the TA range to prevent wrapping.

Parameters

The documentation for this class was generated from the following file: