For a chaser, the difficulties in design of rendezvous and docking controller are mainly reflected by three aspects—stable attitude control of the chaser in the process of orbit control, control of the six degrees of freedom of high-precision relative position and relative attitude in the final approach phase, and the long-term relative position maintenance control at the hold points.
Automatic Control Method and Scheme Design for Rendezvous and Docking
Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods ; Kapitel : 5 ; 219-280
2021-02-17
62 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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