Design of longitudinal control system for a nonlinear F-16 fighter using MSS method

IFAC Proceedings Volumes (IFAC-PapersOnline)

Volumn 16, Issue , 2005, Pages 19-24

  Fung, Eric H K ^a   Wong, Y K ^a   Liu, Hugh H T ^b   Li, Y C ^a  

^a HONG KONG POLYTECHNIC UNIVERSITY   (Hong Kong)

^b UNIVERSITY OF TORONTO   (Canada)

Author keywords

Flight control; Longitudinal control channel; MSS control; Pitch attitude control; Speed control

Indexed keywords

ALTITUDE CONTROL; DESIGN; FLIGHT CONTROL SYSTEMS; FLIGHT SIMULATORS; LONGITUDINAL CONTROL; SATELLITES; SPECIFICATIONS; SPEED CONTROL; SUPERSONIC AIRCRAFT;

AUTOMATIC FLIGHT CONTROL SYSTEMS; CONTROLLER DESIGN METHOD; F-16 FIGHTERS; FAST RESPONSE; FLIGHT CONTROL; NONLINEAR FLIGHT CONTROLS; PITCH ATTITUDE CONTROL; SMOOTH TRANSITIONS;

CONTROLLERS;

EID: 79960707636     PISSN: 14746670     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.3182/20050703-6-cz-1902.01964     Document Type: Conference Paper

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