We consider problems on attitude guidance, navigation and robust gyromoment control of the agile spacecraft for surveying the Earth surface. We present developed methods for dynamic research of the spacecraft attitude control system at the main modes under disturbances and digital control of the gyro moment clusters by the few-excessive gyrodine schemes.
Attitude guidance, navigation and robust control of an agile land-survey satellite
01.06.2017
507331 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Land-survey satellite guidance and attitude control when a scanning stereoscopic imagery
American Institute of Physics | 2018
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