Parametric control to a type of quasi-linear second-order systems via output feedback

被引：26

作者：

Gu, Da-Ke ^{[1
,2
]}

Liu, Guo-Ping ^{[2
,3
]}

Duan, Guang-Ren ^{[3
]}

机构：

[1] Northeast Elect Power Univ, Sch Automat Engn, Jilin, Jilin, Peoples R China

[2] Univ South Wales, Sch Engn, Pontypridd, M Glam, Wales

[3] Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin, Heilongjiang, Peoples R China

来源：

INTERNATIONAL JOURNAL OF CONTROL | 2019年 / 92卷 / 02期

基金：

中国国家自然科学基金;

关键词：

Quasi-linear second-order systems; parametric control; eigenstructure assignment; output feedback; spacecraft rendezvous; EIGENSTRUCTURE ASSIGNMENT;

D O I：

10.1080/00207179.2017.1350885

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper considers the design of output feedback control for a type of quasi-linear second-order systems with the time-varying coefficient matrices containing the state variables and a time-varying parameter vector. Based on the solution to a type of second-order generalised Sylvester matrix equations, general complete parameterisation of a quasi-linear output feedback controller is established with respect to the state variables, the time-varying parameter vector, the constant closed-loop system and another two groups of arbitrary parameters, and also for the left and right closed-loop eigenvectors matrices. With the proposed parametric output feedback control, the closed-loop system can be transformed into a constant linear system with desired eigenstructure. Finally, simulation results are provided to illustrate the convenience and effectiveness of application in the general spacecraft rendezvous problem.

引用

页码：291 / 302

页数：12

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