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Spacecraft attitude control using magnetic actuators
Authors:M. Lovera [Author Vitae]  A. Astolfi [Author Vitae]
Affiliation:a Dipartimento di Elettronica e Informazione, Politecnico di Milano, 32, Piazza Leonardo da Vinci 20133 Milan, Italy
b Department of Electrical and Electronic Engineering, Imperial College, London SW7 2BT, UK
Abstract:The problem of inertial pointing for a spacecraft with magnetic actuators is addressed and an almost global solution to the problem is obtained by means of static attitude and rate feedback. A local solution based on dynamic attitude feedback is also presented. Simulation results demonstrate the practical applicability of the proposed approach.
Keywords:Attitude control   Spacecraft magnetic control   Nonlinear control   Averaging theory
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