STK UtilSend comments on this topic.
AssignEquinoctialRetrograde Method (IAgOrbitState)
See Also
ECoordinateSystem
SemiMajorAxis
H
K
P
Q
MeanLon
Windows





Windows & Linux

Description

Assign a new orbit state using Equinoctial representation.

Syntax

[Visual Basic .NET]
Public Sub AssignEquinoctialRetrograde( _
    ByVal ECoordinateSystem As AgECoordinateSystem, _
    ByVal SemiMajorAxis As Double, _
    ByVal H As Double, _
    ByVal K As Double, _
    ByVal P As Double, _
    ByVal Q As Double, _
    ByVal MeanLon As Double _
)
[C#]
public void AssignEquinoctialRetrograde(
    AgECoordinateSystem ECoordinateSystem,
    double SemiMajorAxis,
    double H,
    double K,
    double P,
    double Q,
    double MeanLon
);
[Managed C++]
public: void AssignEquinoctialRetrograde(
    AgECoordinateSystem ECoordinateSystem,
    double SemiMajorAxis,
    double H,
    double K,
    double P,
    double Q,
    double MeanLon
);
[Unmanaged C++]
public: HRESULT AssignEquinoctialRetrograde(
    AgECoordinateSystem ECoordinateSystem,
    double SemiMajorAxis,
    double H,
    double K,
    double P,
    double Q,
    double MeanLon
);
[Java]
public void assignEquinoctialRetrograde(
    AgECoordinateSystem ECoordinateSystem,
    double SemiMajorAxis,
    double H,
    double K,
    double P,
    double Q,
    double MeanLon
);
[Python - STK API ]
def AssignEquinoctialRetrograde(self, ECoordinateSystem:"AgECoordinateSystem", SemiMajorAxis:float, H:float, K:float, P:float, Q:float, MeanLon:float) -> None:

Parameters

ECoordinateSystem
SemiMajorAxis
H
K
P
Q
MeanLon

See Also

© 2024 Analytical Graphics, Inc. All Rights Reserved.