Non-fragile robust H ∞ control for uncertain spacecraft rendezvous system with pole and input constraints

International Journal of Control

Volumn 85, Issue 7, 2012, Pages 933-941

  Gao, Xiangyu ^a,c   Teo, K L ^a,b   Duan, Guan Ren ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

^b CURTIN UNIVERSITY   (Australia)

^c HEILONGJIANG UNIVERSITY   (China)

Author keywords

input constraint; LMIs; non fragile H control; poles constraint; spacecraft rendezvous system

Indexed keywords

CONTROL DESIGN METHODS; CONTROL PROBLEMS; ILLUSTRATIVE EXAMPLES; INPUT CONSTRAINTS; LINEAR MATRIX INEQUALITY (LMIS); LMI CONSTRAINTS; LMIS; LYAPUNOV THEORIES; NON-FRAGILE; NON-FRAGILE H; NONFRAGILE CONTROLLERS; OPTIMISATIONS; PARAMETER UNCERTAINTY; POLE CONSTRAINTS; ROBUST H; STATE-FEEDBACK CONTROLLERS; SUFFICIENT CONDITIONS;

LINEAR MATRIX INEQUALITIES; POLES;

CONTROLLERS;

EID: 84861533547     PISSN: 00207179     EISSN: 13665820     Source Type: Journal    
DOI: 10.1080/00207179.2012.669848     Document Type: Article

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