Active three-axis attitude control system for a geostationary sa

Aeronautics and astronautics – Spacecraft – Attitude control

Patent

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244171, 364459, B64G 124, B64G 136

Patent

active

050547194

ABSTRACT:
An attitude control system for a stabilized geostationary satellite comprising at least one terrestrial detector (T.sub.1) and a stellar detector oriented towards the North further comprises:

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patent: 4161780 (1979-07-01), Rudolph et al.
patent: 4288051 (1981-09-01), Goschel
patent: 4617634 (1986-10-01), Izumida et al.
patent: 4728061 (1988-03-01), Johnson et al.
patent: 4749157 (1988-06-01), Neufeld
patent: 4767084 (1988-08-01), Chan et al.

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