Magnetic stabilization of a spacecraft and the effect of compensation of information errors

Details Magnetic stabilization of a spacecraft and the effect of compensation of information errors Magnetic stabilization of a spacecraft and the effect of compensation of information errors

Feb 2012

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2012cosre..50...76t&link_type=abstract

Cosmic Research, Volume 50, Issue 1, pp.76-85

Computer Science

Scientific paper

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.

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