Spacecraft automatic rendezvous obstacle avoidance method and system
A technology of spacecraft and equations, applied in control/regulation systems, instruments, non-electric variable control, etc., can solve problems such as redundant description of obstacles and reduction of control accuracy
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[0067] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Apparently, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts all belong to the protection scope of the present invention.
[0068]The object of the present invention is to provide a method and system for automatic rendezvous and obstacle avoidance of spacecraft, which can more accurately control the speed and position of the spacecraft to converge to the target state point, reduce the trajectory error of the spacecraft, and reduce the fuel consumption in the rendezvous process. An automatic rendezvous and obstacle avoidance method based on a suboptimal speed artific...
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