This paper continues the study of the problem on determination of parameters of the spherical motion of a spacecraft and control of this motion using only the Earth magnetic field. The problem of damping the angular velocity of this spacecraft and construction of three-axis orientation regime is solved. An algorithm for estimation of parameters of the spherical motion, which has a wide region of convergence, is proposed.
Control of the spherical motion of a spacecraft in the Earth magnetic field. II. Orientation and stabilization
Journal of Automation and Information Sciences ; 30 , 2-3 ; 39-51
1998
3 Seiten, 17 Quellen
Article (Journal)
English
Spherical Magnetic Dipole Actuator for Spacecraft Attitude Control
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