Generates an external attitude file for a satellite by numerically integrating Euler's equations for the current satellite and save results to the specified file.
[Visual Basic .NET] |
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Public Sub SaveToFile( _ ByVal Filename As String _ ) |
[C#] |
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public void SaveToFile( |
[Managed C++] |
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public: void SaveToFile( |
[Java] |
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public saveToFile( |
[Unmanaged C++] |
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public: HRESULT SaveToFile( |
- Filename