Adaptive fuzzy dynamic surface fault-tolerant control for coupled spacecraft with actuator faults and saturation

被引:2
作者
Mei, Yafei [1 ]
Liao, Ying [1 ]
Gong, Kejie [2 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, 109 Deya Rd, Changsha 410073, Peoples R China
[2] Xian Satellite Control Ctr, Key Lab Fault Diag & Maintenance Spacecraft inorbi, 462 Xianningdong Rd, Xian 710038, Peoples R China
关键词
Lie group SE(3); Coupled spacecraft; Adaptive fuzzy; Dynamic surface; Fault-tolerant control; ATTITUDE-TRACKING CONTROL; PROXIMITY OPERATIONS; RIGID SPACECRAFT; FLEXIBLE SPACECRAFT; STABILIZATION; SATELLITE; MANEUVER;
D O I
10.1016/j.asr.2023.01.053
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This study investigates the fault-tolerant control problem associated with pose tracking for coupled spacecraft in the presence of both actuator faults and actuator saturation constraint. By using the Lie group SE(3), a six-degrees of freedom (6-DOF) coupled kinematics and dynamics model is established to derive the relative motion tracking errors in the exponential coordinates. Then, all system states are reconstructed to develop a dynamic surface fault-tolerant controller. Considering the lumped disturbance consisting of internal uncer-tainties, external unknown disturbances and actuator faults, a fuzzy adaptive method is used to estimate and compensate for the lumped disturbance. Next, the controller is nested with an auxiliary first-order filter to compensate for the saturation constraints. A Lyapunov analysis is used to prove the stability and finite time convergence of the proposed controller. Finally, The tracking performance is verified through a numerical example.(c) 2023 COSPAR. Published by Elsevier B.V. All rights reserved.
引用
收藏
页码:4843 / 4859
页数:17
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