Observer-Based Control for High-Order Fully Actuated Systems

被引:3
|
作者
Zhao, Tianyi [1 ]
Duan, Guangren [2 ]
Xin, Wanqing [3 ]
机构
[1] China Acad Launch Vehicle Technol, Beijing Inst Aerosp Syst Engn, Beijing 100076, Peoples R China
[2] Southern Univ Sci & Technol, Ctr Control Sci & Technol, Shenzhen 518055, Peoples R China
[3] China Acad Launch Vehicle Technol, Beijing 100076, Peoples R China
基金
中国国家自然科学基金;
关键词
Observer-based control; nonlinear control; high-order fully actuated systems; exponential stability; flexible spacecraft control; FEEDFORWARD NONLINEAR-SYSTEMS; OUTPUT-FEEDBACK CONTROL; TRACKING CONTROL; LMI CONDITIONS; DESIGN; LIPSCHITZ;
D O I
10.1109/ACCESS.2023.3335224
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
An observer-based control method for high-order fully actuated systems is proposed. First, a concept of exponentially stable observers is introduced, which, different from traditional state observers, requires not only asymptotic convergence of observation errors, but also exponential convergence. Further, inspired by existing results, two design methods for exponentially stable observers are developed, one of which is less conservative and the other is simpler and more straightforward to use. Secondly, a parametric control method based on the exponentially stable observer is proposed, which ensures the exponential stability of the closed-loop system. Moreover, the proposed method does not rely on the solution of nonlinear partial differential equations, and although the system is nonlinear and time-varying, the Separation Principle still holds under this control strategy, which is a significant advantage of the proposed method. Finally, the method is applied to the attitude control of flexible spacecraft with nonlinear inertia, and comparative simulation results verify the effect of the proposed approach.
引用
收藏
页码:132239 / 132253
页数:15
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