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SimpleAscentPropagatorMixedFixedPositionAndInertialVelocityToMotionFixed Method

This method computes the burnout motion in the fixed frame of the CentralBody from mixed inertial velocity/fixed position input.

Namespace:  AGI.Foundation.Propagators
Assembly:  AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 25.1.421.0 (25.1.421.0)
Syntax
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public static Motion<Cartesian> MixedFixedPositionAndInertialVelocityToMotionFixed(
	bool isAtPole,
	KinematicTransformation inertialToFixed,
	Cartesian position,
	double inertialSpeed,
	double inertialFlightPathAngle,
	double inertialAzimuth
)

Parameters

isAtPole
Type: SystemBoolean
Indicates whether the position vector is at a pole of the central body ellipsoid.
inertialToFixed
Type: AGI.Foundation.CoordinatesKinematicTransformation
The transformation from the inertial reference frame to the fixed reference frame.
position
Type: AGI.Foundation.CoordinatesCartesian
The position of the launch vehicle in the CentralBody's fixed frame at burnout time.
inertialSpeed
Type: SystemDouble
The speed in the inertial frame.
inertialFlightPathAngle
Type: SystemDouble
The flight path angle in the inertial frame.
inertialAzimuth
Type: SystemDouble
The angle from North at the burnout position.

Return Value

Type: MotionCartesian
A MotionT representing the burnout state in the fixed frame.
See Also