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KIAM Preprint № 22, Moscow, 2015
Authors: Ovchinnikov M. Y., Roldugin D. S.
Dual-spin satellite angular motion in magnetic and gravitational fields
Attitude motion of a satellite equipped with single flywheel and active magnetic attitude control system is considered. Time-response of the system in transient mode is studied. Characteristic exponent approximations values are obtained. Small steady-state motion near the gravitational attitude is considered. Accuracy and time-response is studied. An algorithm of arbitrary but given attitude in the orbital plane is proposed and studied. Numerical analysis is carried out.
magnetic attitude control system, flywheel, dual spin
Publication language: russian/english, pages: 23/20
Research direction:
Theoretical and applied problems of mechanics
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