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] |
---|
Public Sub SaveToFile( _ ByVal Filename As String _ ) |
[C#] |
---|
public void SaveToFile( string Filename ); |
[Managed C++] |
---|
public: void SaveToFile( String __gc ^ Filename ); |
[Unmanaged C++] |
---|
public: HRESULT SaveToFile( BSTR Filename ); |
[Java] |
---|
public void saveToFile( String Filename ); |
[Python - STK API ] |
---|
def SaveToFile(self, Filename:str) -> None: |
- Filename