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Reduced-Order Fixed-Time Control for Under-actuated Spacecra...

Reduced-Order Fixed-Time Control for Under-actuated Spacecraft Hovering

作     者:Yi Cao Zhijun Chen Yuzhu Bai Yong Zhao 

作者单位:College of Aerospace Science and Engineering National University of Defense Technology 

会议名称:《第40届中国控制会议》

会议日期:2021年

学科分类:08[工学] 081105[工学-导航、制导与控制] 0802[工学-机械工程] 0811[工学-控制科学与工程] 080201[工学-机械制造及其自动化] 

关 键 词:Under-actuated Spacecraft Hovering Fixed-Time Control Reduced-Order Control 

摘      要:This paper proposes a Reduced-Order Fixed-Time Control(ROFTC) method for the hovering problem of the under-actuated spacecraft. Firstly, the dynamic equation of the under-actuated relative motion is established for the hovering mission of the under-actuated spacecraft, and the controllability of the system and the feasible set of hovering are analyzed. Then,under-actuated relative motion model is deduced by dimensionality reduction. Based on the reduced-order dynamics model, a fixed-time controller is proposed. The simulation results show that the under-actuated spacecraft can achieve hovering motion to the given position under the reduced-order fixed-time controller, and the system state can converge in a fixed time with high accuracy.

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