The invention relates to a tethered satellite in-plane angle control method based on a swing direction. The tethered satellite in-plane angle control method comprises the following steps: a tethered satellite system controls a tethered satellite in-plane angle by taking a rope winding and unwinding speed # imgabs0 # as a control variable; the rope winding and unwinding speed # imgabs1 # comprises two parts, the first part is theoretical rope speed # imgabs2 #, the second part is rope speed feedback quantity u, the sign of the rope speed feedback quantity u is opposite to the sign of the in-plane angular speed # imgabs3 # collected in real time, and the rope speed feedback quantity u is used for eliminating external disturbing force and swing caused when the theoretical rope speed # imgabs4 # is adopted for open-loop rope winding and unwinding.
本发明涉及一种基于摆动方向的绳系卫星面内角控制方法:绳系卫星系统以收放绳速度#imgabs0#为控制变量,控制绳系卫星面内角;所述收放绳速度#imgabs1#包括两部分:第一部分为理论绳速#imgabs2#第二部分为绳速反馈量u,所述绳速反馈量u的符号与实时采集的绳系卫星面内角速度#imgabs3#的符号相反,用于消除外部扰动力以及采用理论绳速#imgabs4#开环收放绳时引起的摆动。
Method for controlling in-plane angle of tethered satellite based on swinging direction
一种基于摆动方向的绳系卫星面内角控制方法
2024-08-02
Patent
Electronic Resource
Chinese
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