STABILIZATION OF A CLASS OF HYBRID SYSTEMS ARISING IN FLEXIBLE SPACECRAFT

被引：24

作者：

BISWAS, SK

AHMED, NU

机构：

[1] Univ of Ottawa, Ottawa, Ont, Can, Univ of Ottawa, Ottawa, Ont, Can

来源：

JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS | 1986年 / 50卷 / 01期

关键词：

CONTROL SYSTEMS - Theory - MATHEMATICAL TECHNIQUES - Differential Equations - SYSTEM STABILITY;

D O I：

10.1007/BF00938479

中图分类号：

C93 [管理学]; O22 [运筹学];

学科分类号：

070105 ; 12 ; 1201 ; 1202 ; 120202 ;

摘要：

We consider the problem of rigorous modeling of flexible spacecraft and their stabilization. It is shown that the dynamics of the flexible spacecraft can be described by a coupled system of ordinary differential equations and partial differential equations (hybrid system). Lyapunov's approach is used to prove the stabilizability of the system. Simple feedback controls are suggested for stabilization of flexible spacecraft.

引用

页码：83 / 108

页数：26

共 21 条

[1]

Ahmed N. U., 1981, OPTIMAL CONTROL DIST

[2] STABILITY ANALYSIS OF A TRANSMISSION-LINE WITH VARIABLE PARAMETERS [J].