On-orbit debugging method for unbalanced amplitude and phase of large-inertia rotating part of satellite

The invention discloses an on-orbit debugging method for unbalance amplitude and phase of a large-inertia rotating part of a satellite, and aims to solve the problem that periodic disturbance torque caused by unbalance of the rotating part is difficult to directly compensate by an attitude and orbit...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LU LIN, LU QIDONG, NIE ZHANGHAI, XU PENG, ZHANG ZILONG, LU DANPING, PENG RUI, XU ZIYAO, ZUO ZHIDAN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR
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