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Attitude Stabilization of a Satellite by Magnetic Coils
by
Vladimir A. Bushenkov
University of Evora, Portugal
Coauthors: Michael Yu. Ovchinnikov (Keldysh Institute of Applied Mathematics, Moscow, Russia), Georgi V. Smirnov (University of Porto, Portugal)
Stabilization problem for a satellite is considered. The only measurement is of the magnetic field in the satellite coordinates. The control is carried out by a magnetic moment of current coils (magnetorquers) mounted on the satellite body. The stabilizer constructed in this work solves the problems of magnetic and gravitational stabilization. Results of numerical simulation are presented.
Date received: January 11, 2000
Copyright © 2000 by the author(s). The author(s) of this document and the organizers of the conference have granted their consent to include this abstract in Atlas Conferences Inc. Document # cadd-15.