Dynamic surface control of constrained hypersonic flight models with parameter estimation and actuator compensation

Asian Journal of Control

Volumn 16, Issue 1, 2014, Pages 162-174

  Xu, Bin ^a,b   Huang, Xiyuan ^c   Wang, Danwei ^b   Sun, Fuchun ^d  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

^b NANYANG TECHNOLOGICAL UNIVERSITY   (Singapore)

^c CHINA ACADEMY OF LAUNCH VEHICLE TECHNOLOGY   (China)

^d TSINGHUA UNIVERSITY   (China)

Author keywords

dynamic surface control; Hypersonic flight vehicle; input saturation; linearly parameterized form

Indexed keywords

CLOSED LOOP SYSTEMS; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; INVERSE PROBLEMS; PARAMETER ESTIMATION; UNCERTAINTY ANALYSIS;

CONTROL ORIENTED MODELS; DYNAMIC INVERSE CONTROLS; DYNAMIC SURFACE CONTROL; HYPERSONIC FLIGHT VEHICLES; INPUT SATURATION; LONGITUDINAL DYNAMICS; PARAMETERIZED; ROBUST ADAPTIVE CONTROLLER;

CONTROLLERS;

EID: 84880918925     PISSN: 15618625     EISSN: 19346093     Source Type: Journal    
DOI: 10.1002/asjc.679     Document Type: Article

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