Rotational motion control of a spacecraft

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Rotational motion control of a spacecraft

This note describes a systematic procedure for the control synthesis of a rigid spacecraft using the energy shaping method. The geometric concept of a mechanical system in a coordinate-independent form is used to derive a control algorithm for the Euler–Poincaré equations. The main result of this note is a specialization of the method on the unit quaternion group. This note is concluded with th...

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ژورنال

عنوان ژورنال: IEEE Transactions on Automatic Control

سال: 2003

ISSN: 0018-9286

DOI: 10.1109/tac.2003.809781