Abstract The system of spacecraft angular stabilization of middle accuracy rating and with magnetic executive devices is considered. A three-axis magnetometer is used as a single sensitive element of the subsystem of attitude determination. Combination of specific features of the control law and the algorithm of attitude determination allows one to realize a sufficiently reliable stabilization system of simple design, which is rather economical, as far as computing time is concerned.
Magnetic stabilization of a spacecraft and the effect of compensation of information errors
Cosmic Research ; 50 , 1 ; 76-85
2012-02-01
10 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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