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 _
)
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[C#] |
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public void SaveToFile(
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[Managed C++] |
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public: void SaveToFile(
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[Java] |
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public saveToFile(
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[Unmanaged C++] |
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public: HRESULT SaveToFile(
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- Filename