Assign a new orbit state using Classical representation.
[Visual Basic .NET] |
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Public Sub AssignClassical( _ ByVal ECoordinateSystem As AgECoordinateSystem, _ ByVal SemiMajorAxis As Double, _ ByVal Eccentricity As Double, _ ByVal Inclination As Double, _ ByVal ArgOfPerigee As Double, _ ByVal RAAN As Double, _ ByVal MeanAnomaly As Double _ ) |
[C#] |
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public void AssignClassical( AgECoordinateSystem ECoordinateSystem, double SemiMajorAxis, double Eccentricity, double Inclination, double ArgOfPerigee, double RAAN, double MeanAnomaly ); |
[Managed C++] |
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public: void AssignClassical( AgECoordinateSystem ECoordinateSystem, double SemiMajorAxis, double Eccentricity, double Inclination, double ArgOfPerigee, double RAAN, double MeanAnomaly ); |
[Unmanaged C++] |
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public: HRESULT AssignClassical( AgECoordinateSystem ECoordinateSystem, double SemiMajorAxis, double Eccentricity, double Inclination, double ArgOfPerigee, double RAAN, double MeanAnomaly ); |
[Java] |
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public void assignClassical( AgECoordinateSystem ECoordinateSystem, double SemiMajorAxis, double Eccentricity, double Inclination, double ArgOfPerigee, double RAAN, double MeanAnomaly ); |
[Python - STK API ] |
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def AssignClassical(self, ECoordinateSystem:"AgECoordinateSystem", SemiMajorAxis:float, Eccentricity:float, Inclination:float, ArgOfPerigee:float, RAAN:float, MeanAnomaly:float) -> None: |
- ECoordinateSystem
- SemiMajorAxis
- Eccentricity
- Inclination
- ArgOfPerigee
- RAAN
- MeanAnomaly