On the possibility of long-term maintenance of geostationary satellite attitude without using the external information sensors and inertial sensors

Details On the possibility of long-term maintenance of geostationary satellite attitude without using the external information sensors and inertial sensors On the possibility of long-term maintenance of geostationary satellite attitude without using the external information sensors and inertial sensors

Jun 2009

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2009cosre..47..235p&link_type=abstract

Cosmic Research, Volume 47, Issue 3, pp.235-242

Physics

45.40.Cc

Scientific paper

The problem of maintaining spacecraft attitude during the loss of information from attitude sensors and inertial sensors is considered. The problem is solved on the basis of the force gyro stabilization principle with producing an angular momentum in the plane of orbit. The redundant mode of attitude maintenance is developed for spacecraft of the Yamal series. The results of testing the mode during the in-flight tests of the Yamal-200 spacecraft are presented.

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