Attitude and orbit control semi-physical simulation method and system for satellite constellation

The invention provides an attitude and orbit control semi-physical simulation method and simulation system for a satellite constellation. The satellite constellation comprises a plurality of satellites, each satellite comprises at least one attitude sensor and at least one execution mechanism, and t...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	XIE XIANGHUA, YANG GUANG, YANG WENZHE, YAN LINGLING, DAI ZHENGSHENG, BIAN JING, ZHU YE, HUANG ZHIWEI, HE XIAWEI
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING
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