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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
Abstract:
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.
Keywords:
magnetic attitude control system, flywheel, dual spin
Publication language: russian/english,  страниц: 23 / 20
Research direction:
Theoretical and applied problems of mechanics
Russian source text: English source text:
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