LFT approach to autopilot design for missiles

Proceedings of the American Control Conference

Volumn 5, Issue , 1995, Pages 2990-2994

  Huang, Yun ^a   Lu, Wei Min ^a  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CONTROL NONLINEARITIES; CONTROL SYSTEM SYNTHESIS; DISCRETE TIME CONTROL SYSTEMS; FEEDBACK CONTROL; LINEAR CONTROL SYSTEMS; MATHEMATICAL TRANSFORMATIONS; MATRIX ALGEBRA; MISSILES; ROBUSTNESS (CONTROL SYSTEMS);

FEEDBACK LOOPS; LINEAR FRACTIONAL TRANSFORMATION; LINEAR MATRIX INEQUALITIES; TAILFIN CONTROLLED MISSILE;

CONTROL THEORY;

EID: 0029201253     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)