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KIAM Preprint  133, Moscow, 2016
Authors: Ovchinnikov M. Y., Roldugin D. S., Tkachev S. S.
Study of the accuracy of active magnetic damping algorithm
Attitude motion of a satellite equipped with an active magnetic attitude control system is considered. Control system implements -Bdot damping algorithm. Satellite behavior is analyzed in a steady-state motion. Slow spinning around the principal axis of maximum inertia is proven, angular velocity is found. Attitude accuracy in dipole geomagnetic field model is studied. Numerical analysis is carried out.
magnetic attitude control system, damping, Bdot
Publication language: russian/english, pages: 19/16
Research direction:
Theoretical and applied problems of mechanics
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