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AssignClassical Method (IAgOrbitState)
See Also
ECoordinateSystem
SemiMajorAxis
Eccentricity
Inclination
ArgOfPerigee
RAAN
MeanAnomaly
Windows





Windows & Linux

Description

Assign a new orbit state using Classical representation.

Syntax

[Visual Basic .NET]
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#]
public void AssignClassical(
    AgECoordinateSystem ECoordinateSystem,
    double SemiMajorAxis,
    double Eccentricity,
    double Inclination,
    double ArgOfPerigee,
    double RAAN,
    double MeanAnomaly
);
[Managed C++]
public: void AssignClassical(
    AgECoordinateSystem ECoordinateSystem,
    double SemiMajorAxis,
    double Eccentricity,
    double Inclination,
    double ArgOfPerigee,
    double RAAN,
    double MeanAnomaly
);
[Unmanaged C++]
public: HRESULT AssignClassical(
    AgECoordinateSystem ECoordinateSystem,
    double SemiMajorAxis,
    double Eccentricity,
    double Inclination,
    double ArgOfPerigee,
    double RAAN,
    double MeanAnomaly
);
[Java]
public void assignClassical(
    AgECoordinateSystem ECoordinateSystem,
    double SemiMajorAxis,
    double Eccentricity,
    double Inclination,
    double ArgOfPerigee,
    double RAAN,
    double MeanAnomaly
);
[Python - STK API ]
def AssignClassical(self, ECoordinateSystem:"AgECoordinateSystem", SemiMajorAxis:float, Eccentricity:float, Inclination:float, ArgOfPerigee:float, RAAN:float, MeanAnomaly:float) -> None:

Parameters

ECoordinateSystem
SemiMajorAxis
Eccentricity
Inclination
ArgOfPerigee
RAAN
MeanAnomaly

See Also

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