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CircularEquatorialOrbitGrazingAngleConstraintDetermineLimitPointsForOccultationArcs Method

Determines the end points on a circular equatorial orbit with the provided radius of the portions of the orbit which transit or are occulted by the ellipsoid as viewed from the provided position.

Namespace:  AGI.Foundation.Access.Constraints
Assembly:  AGI.Foundation.Platforms (in AGI.Foundation.Platforms.dll) Version: 24.3.420.0 (24.3.420.0)
Syntax
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public static List<Cartesian> DetermineLimitPointsForOccultationArcs(
	Ellipsoid ellipsoid,
	double radius,
	Cartesian position
)

Parameters

ellipsoid
Type: AGI.Foundation.Geometry.ShapesEllipsoid
The ellipsoidal shape of the central body.
radius
Type: SystemDouble
The radius of the circular equatorial orbit.
position
Type: AGI.Foundation.CoordinatesCartesian
The starting point of the directed line segment.

Return Value

Type: ListCartesian
The points on the circular equatorial orbit.
Remarks
Input and output vectors are assumed to be in the fixed frame of the central body.
See Also