Mixed H2/H∞ attitude control of a LEO microsatellite in the presence of inertia matrix uncertainty

Proceedings of the American Control Conference

Volumn 2, Issue , 2002, Pages 1354-1359

  Sun, Yun Ping ^a   Yang, Ciann Dong ^a  

^a CHENG SHIU UNIVERSITY   (Taiwan)

Author keywords

Linear matrix inequality; Microsatellite attitude control; Mixed H2 H control

Indexed keywords

COMPUTATIONAL COMPLEXITY; CONTROL SYSTEM SYNTHESIS; FEEDBACK CONTROL; MATRIX ALGEBRA; ORBITS; POSITION CONTROL; ROBUSTNESS (CONTROL SYSTEMS); SATELLITES; STATE FEEDBACK; SYSTEM STABILITY; TORQUE CONTROL; UNCERTAIN SYSTEMS;

ATTITUDE CONTROL; LINEAR MATRIX INEQUALITY; LOW EARTH ORBIT; MICROSATELLITE; MOMENT OF INERTIA; ROOT MEAN SQUARE;

OPTIMAL CONTROL SYSTEMS;

EID: 0036061420     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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