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Spacecraft autonomous fly-around multi-mode control based on hybrid state machine
Received date: 2022-11-21
Revised date: 2022-11-28
Accepted date: 2022-12-07
Online published: 2022-12-14
Supported by
National Natural Science Foundation of China(U21B6001)
This paper investigates the autonomous control problem for non-cooperative targets, and proposes a multi-mode control approach based on the hybrid state machine. First, according to the task objective of fly-around and orbit safety analysis, we define six states including long-range guidance, close-range guidance, relative-position keeping, fly-around transfer, collision threat avoidance, and evacuation. Moreover, the control objective of each state is designed. Second, to achieve the coordinated transitions and control between the states, a state monitoring and management approach is developed and state transition functions designed based on the finite state machine. A novel multi-mode motion plan and adaptive finite-time control strategies are then proposed to guarantee the tracking performance according to the task objective. Finally, the proposed autonomous fly-around control approach is simulated by digital simulation software, and the simulation results show the effectiveness of the proposed approach.
Min LI , Li YUAN , Chunling WEI . Spacecraft autonomous fly-around multi-mode control based on hybrid state machine[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023 , 44(18) : 328296 -328296 . DOI: 10.7527/S1000-6893.2022.28296
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