Robust attitude control of flexible spacecraft with quality characteristic parameter uncertainty

2010 8th IEEE International Conference on Control and Automation, ICCA 2010

Volumn , Issue , 2010, Pages 486-491

  Yanru, Zhou ^a   Xiaoqi, Shen ^a   Jianping, Zeng ^a   Hongfei, Sun ^a  

^a XIAMEN UNIVERSITY   (China)

Author keywords

Attitude control; Dynamic output feedback; Flexible; Quality characteristic parameter uncertainty; Variable substitution method

Indexed keywords

CONTROL PROBLEMS; DYNAMIC OUTPUT FEEDBACK; DYNAMIC OUTPUT FEEDBACK CONTROLLER; EXTERNAL DISTURBANCES; FLEXIBLE; LINEARIZATION METHODS; LMI TOOLBOXES; NON-LINEAR MATRIX INEQUALITY; QUALITY CHARACTERISTIC; QUALITY CHARACTERISTIC PARAMETER UNCERTAINTY; ROBUST ATTITUDE CONTROLLER; SATELLITE ATTITUDE CONTROL; SIMULATION RESULT; STANDARD H; VARIABLE SUBSTITUTION;

ATTITUDE CONTROL; CONTROLLERS; DISTRIBUTED PARAMETER CONTROL SYSTEMS; FEEDBACK LINEARIZATION; FLEXIBLE SPACECRAFT; LINEAR MATRIX INEQUALITIES; NAVIGATION; NONLINEAR FEEDBACK; SPATIAL VARIABLES CONTROL;

QUALITY CONTROL;

EID: 77957875734     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ICCA.2010.5524240     Document Type: Conference Paper

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