Contemporary land-survey mini-satellites have general mass up to 500 kg and are placed onto the orbit altitudes up to 800 km. For such spacecraft some principle problems on optimal attitude guidance and robust control are considered and elaborated methods are presented for their solving.
Attitude guidance and control of land-survey mini-satellite
01.06.2015
930947 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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