Direct neural discrete control of hypersonic flight vehicle

Nonlinear Dynamics

Volumn 70, Issue 1, 2012, Pages 269-278

  Xu, Bin ^a,b,c   Wang, Danwei ^a   Sun, Fuchun ^b   Shi, Zhongke ^c  

^a NANYANG TECHNOLOGICAL UNIVERSITY   (Singapore)

^b TSINGHUA UNIVERSITY   (China)

^c NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Back stepping; Discrete time; Hypersonic flight vehicle; Neural network

Indexed keywords

CONTROL GAINS; CONTROLLER DESIGNS; DIRECT NEURAL NETWORKS; DISCRETE CONTROL; DISCRETE-TIME; ERROR FEEDBACK; FLIGHT PATH ANGLE; HYPERSONIC FLIGHT VEHICLES; NEURAL CONTROL; NN CONTROL; PATH ANGLES; PITCH ANGLE; PITCH RATE; SEMI-GLOBAL; SIMULATION EXAMPLE; SYSTEM UNCERTAINTIES; UNIFORM ULTIMATE BOUNDEDNESS; UPPER BOUND;

HYPERSONIC AERODYNAMICS; NEURAL NETWORKS;

CONTROLLERS;

EID: 84867900152     PISSN: 0924090X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11071-012-0451-x     Document Type: Article

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