Reliable Aircraft Flight Control Using Static Output-Feedback

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Liao, Fang ^a   Wang, Jian Liang ^a   Yang, Guang Hong ^b  

^a NANYANG TECHNOLOGICAL UNIVERSITY   (Singapore)

^b NATIONAL UNIVERSITY OF SINGAPORE   (Singapore)

Author keywords

Affine quadratic stability performance test; Control surface impairment; LMI; Reliable aircraft control; Static output feedback; Tracking

Indexed keywords

AIRCRAFT; AIRCRAFT CONTROL; AIRCRAFT DETECTION; CONTROL SURFACES; DESIGN; FEEDBACK CONTROL; FLIGHT SIMULATORS; LINEAR MATRIX INEQUALITIES; LINEAR SYSTEMS; SURFACE DISCHARGES;

AFFINE PARAMETERS; AIRCRAFT FLIGHT CONTROL; DESIGN AND SIMULATION; FLIGHT CONTROLLERS; QUADRATIC STABILITY; STATIC OUTPUT; STATIC OUTPUT FEEDBACK; TRACKING CONTROLLER;

CONTROLLERS;

EID: 85132917925     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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