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Optimal Discrete-Time Design of Three-Axis Magnetic Attitude Control Laws

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3 Author(s)
Pulecchi, Tiziano ; Dipt. di Elettron. e Inf., Politec. di Milano, Milan, Italy ; Lovera, M. ; Varga, A.

The problem of designing discrete-time attitude controllers for three-axis stabilization of magnetically actuated spacecraft is considered. Several methods are discussed and an approach to the tuning of various classes of projection-based controllers is proposed relying on periodic optimal output feedback control techniques. The main advantages of the proposed methods are discussed and illustrated in a simulation study.

Published in:

Control Systems Technology, IEEE Transactions on  (Volume:18 ,  Issue: 3 )