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Three Axes Attitude Stabilization of Geostationary Satellite during Apogec orbit Maneuvering
Pages: 7-15+6
Year: Issue:  2
Journal: Aerospace Control

Keyword:  Solar arrayFlexibilityThree axes stabilization;
Abstract: A dynamics model including rigid, liquid sloshing and flexible solar array dynamics of three axis stabilized geostationary satellite during apogee orbit maneuver is provided in the paper. The model has proved valid pass through the practice satellite control design. A Type of controller which is consisted by PID. plexible solar array filters and sloshing filters is given. The design specification has been satisficed by the controller, and it is simple and reliable. Finally simulation and stability analysis results are provided.
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