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LambertOrbitSolverSolveFixedDurationTransfer Method (Cartesian, Cartesian, Duration, Int32, LambertPathType, OrbitDirectionType)

Solves the classic Lambert problem with the specified number of revolutions.

Namespace:  AGI.Foundation.Propagators
Assembly:  AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.2.419.0 (24.2.419.0)
Syntax
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public LambertResult SolveFixedDurationTransfer(
	Cartesian initialPosition,
	Cartesian finalPosition,
	Duration timeOfFlight,
	int numberOfRevolutions,
	LambertPathType pathType,
	OrbitDirectionType directionOfFlight
)

Parameters

initialPosition
Type: AGI.Foundation.CoordinatesCartesian
The starting position of the orbit/transfer.
finalPosition
Type: AGI.Foundation.CoordinatesCartesian
The ending position of the orbit/transfer.
timeOfFlight
Type: AGI.Foundation.TimeDuration
The Duration taken between the initial and final points.
numberOfRevolutions
Type: SystemInt32
The number of revolutions to reach the final position.
pathType
Type: AGI.Foundation.PropagatorsLambertPathType
Specifies whether the Lambert algorithm should take the smaller or large semi-major axis path when the revolution count is greater than 0.
directionOfFlight
Type: AGI.Foundation.CoordinatesOrbitDirectionType
Determines if the flight path is prograde or retrograde.

Return Value

Type: LambertResult
The motion at the initial and final positions and the time of flight.
Remarks
This method does not include an orbital plane vector used for transfers spanning π in angle subtended.
See Also