BallisticPropagatorConfigureFromApogeeAltitude Method (Cartesian, Double)

Populates the InitialVelocity and FinalTime values for the trajectory which, at apogee, reaches the specified altitude.

Namespace: AGI.Foundation.Propagators
Assembly: AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.3.420.0 (24.3.420.0)

Syntax

C++

Copy

public BallisticPropagatorSolutionType ConfigureFromApogeeAltitude(
	Cartesian targetPositionFixed,
	double apogeeAltitude
)

Public Function ConfigureFromApogeeAltitude ( 
	targetPositionFixed As Cartesian,
	apogeeAltitude As Double
) As BallisticPropagatorSolutionType

public:
BallisticPropagatorSolutionType ConfigureFromApogeeAltitude(
	Cartesian targetPositionFixed, 
	double apogeeAltitude
)

member ConfigureFromApogeeAltitude : 
        targetPositionFixed : Cartesian * 
        apogeeAltitude : float -> BallisticPropagatorSolutionType

Parameters

targetPositionFixed: Type: AGI.Foundation.CoordinatesCartesian
The target position in the CentralBody's fixed frame.
apogeeAltitude: Type: SystemDouble
The desired altitude of the trajectory's apogee, in meters.

Return Value

Type: BallisticPropagatorSolutionType
An enumeration which reports whether the calculation successfully met the provided constraint, or contains an alternative solution or best guess.

Reference

BallisticPropagator Class

ConfigureFromApogeeAltitude Overload

AGI.Foundation.Propagators Namespace

BallisticPropagatorAddLanguageSpecificTextSet("LSTE9AE6289_0?cpp=::|nu=.");ConfigureFromApogeeAltitude Method (Cartesian, Double)

Parameters

Return Value

Reference

BallisticPropagatorConfigureFromApogeeAltitude Method (Cartesian, Double)