Constrained Fixed-Time Terminal Sliding-Mode Control With Prescribed Performance for Space Manipulator System

被引:1
|
作者
Hu, Meiling [1 ]
Yang, Xuebo [1 ,2 ]
Dong, Hanlin [3 ]
机构
[1] Harbin Inst Technol, Res Inst Intelligent Control & Syst, Harbin 150001, Peoples R China
[2] State Key Lab Robot & Syst, Harbin 150001, Peoples R China
[3] Northwestern Polytech Univ, Sch Automat, Xian 710129, Peoples R China
关键词
Fasteners; Manipulator dynamics; Aerodynamics; Uncertainty; Convergence; Trajectory tracking; Space vehicles; Fixed-time terminal sliding-mode control (FTSMC); input constraints; prescribed performance; radial basis function neural network (RBFNN) approximation; screw theory; MIMO NONLINEAR-SYSTEMS; ADAPTIVE-CONTROL; TRACKING CONTROL; STABILIZATION; DESIGN; ROBOTS;
D O I
10.1109/TAES.2023.3333809
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article focuses on the high-precision position tracking problem for the free-float space manipulator (FFSM) system subject to parametric uncertainties, input saturation, and state constraints. To this end, the screw-based dynamics using the Newton-Euler iterative method, with a global and unique attitude representation, are established; then, a chattering-free fixed-time sliding-mode control (FTSMC) scheme is developed based on the proposed dynamics model. A radial basis function neural network (RBFNN) with proper hidden layers and nodes is integrated into the proposed controller, while modeling approximation errors are well-inhibited by adaptive laws. Since the tracking error has been explicitly constrained by an exponential decay function, the Lyapunov analysis indicates that the transient and steady performance and state constraints can be guaranteed simultaneously. Simulation experiments taking an FFSM with six-degree-of-freedom (DOF) illustrate the effectiveness of the proposed control scheme from two aspects: joint-space positioning and trajectory tracking.
引用
收藏
页码:1074 / 1090
页数:17
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