Active self-stabilization control method for attitude of spacecraft in orbit virtual field

The invention discloses a spacecraft attitude active self-stabilization control method for an orbit virtual field, and the method specifically comprises the following steps: extrapolating the position and speed of a spacecraft orbit through the GNSS data of a current spacecraft; calculating the spac...

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Bibliographische Detailangaben
Hauptverfasser: WU SHENGGANG, SHEN SHILU, CHEN DAN, ZHU YONGJIE, AN YUAN, YANG BIAO, KONG BO, JIANG YU, ZHANG ZHUO, TAI NENGJIAN
Format: Patent
Sprache:chi ; eng
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