Missile reaction-jet/aerodynamic compound control system design based on adaptive sliding mode control and fuzzy logic

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 29, Issue 1, 2008, Pages 165-169

  Dong, Chaoyang ^a   Wang, Feng ^a   Gao, Xiaoying ^b   Wang, Qing ^a  

^a BEIHANG UNIVERSITY   (China)

^b BEIJING AEROSPACE AUTOMATIC CONTROL INSTITUTE   (China)

Author keywords

Adaptive sliding mode control; Fuzzy logic; Genetic algorithm; Reaction jet aerodynamic compound control

Indexed keywords

AERODYNAMICS; FUZZY INFERENCE; FUZZY LOGIC; GENETIC ALGORITHMS; MISSILES;

EXTERNAL DISTURBANCES; PARAMETRIC PERTURBATIONS; REACTION JET CONTROL SUBSYSTEM (RCS); RESPONSE SPEED;

SLIDING MODE CONTROL;

EID: 40449107727     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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