Linear parameter varying approach to gain scheduled missile autopilot design

Proceedings of the American Control Conference

Volumn 2, Issue , 1992, Pages 1317-1321

  Shamma, Jeff S ^a   Cloutier, James R ^a  

^a UNIVERSITY OF TEXAS AT AUSTIN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION CONTROL; ANGLE OF ATTACK INDICATORS; AUTOMATIC PILOTS; CONTROL EQUIPMENT; CONTROL NONLINEARITIES; CONTROL SYSTEM SYNTHESIS; DESIGN; DISTRIBUTED PARAMETER CONTROL SYSTEMS; DYNAMICS; FLIGHT DYNAMICS; LINEAR CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS);

ANGLE OF ATTACK; GAIN SCHEDULED DESIGN; MISSILE LONGITUDINAL AUTOPILOT; QUASI LINEAR PARAMETER VARYING (LPV) FORM;

MISSILES;

EID: 0027065895     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)