作者: Zhu Wenshan , Cai Chensheng , Zha Li , Du Ning , Niu Rui
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摘要: The invention discloses a jet control method based on quaternion information, which achieves maneuver conversion to an earth orientation of satellite in sun oriented safety mode, namely the recapture control. comprises following steps of: S1, describing attitude for three-axis switching from current target with quaternion; S2, resolving angular velocity vector relative orbital coordinate system gyroscope combined information; and S3, designing algorithm achieve shortest path satellite. disclosed by has advantages that through description deviation between reference quaternion, calling algorithm, is achieved, flow simplified, time required shortened.