Assign a new orbit state using Equinoctial representation.
[Visual Basic .NET] |
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Public Sub AssignEquinoctialPosigrade( _ 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#] |
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public void AssignEquinoctialPosigrade( AgECoordinateSystem ECoordinateSystem, double SemiMajorAxis, double H, double K, double P, double Q, double MeanLon ); |
[Managed C++] |
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public: void AssignEquinoctialPosigrade( AgECoordinateSystem ECoordinateSystem, double SemiMajorAxis, double H, double K, double P, double Q, double MeanLon ); |
[Unmanaged C++] |
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public: HRESULT AssignEquinoctialPosigrade( AgECoordinateSystem ECoordinateSystem, double SemiMajorAxis, double H, double K, double P, double Q, double MeanLon ); |
[Java] |
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public void assignEquinoctialPosigrade( AgECoordinateSystem ECoordinateSystem, double SemiMajorAxis, double H, double K, double P, double Q, double MeanLon ); |
[Python - STK API ] |
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def AssignEquinoctialPosigrade(self, ECoordinateSystem:"AgECoordinateSystem", SemiMajorAxis:float, H:float, K:float, P:float, Q:float, MeanLon:float) -> None: |
- ECoordinateSystem
- SemiMajorAxis
- H
- K
- P
- Q
- MeanLon