DocumentCode
3575738
Title
A dynamic inverse control law for hypersonic vehicles based on fuzzy logic
Author
Wang Jian ; Yao Li
Author_Institution
Beijing Aerosp. Autom. Control Inst., Beijing, China
fYear
2014
Firstpage
439
Lastpage
442
Abstract
An integrated control law is presented considering a nonlinear model of generic hypersonic vehicle as a plant. Based on dynamic inverse theory, the nonlinear model is transformed into an equivalent affine system. Then a dynamic inverse controller could be designed according to the equivalent system. What´s more, two fuzzy logic regulars are used to adapt control parameters on line, and the fuzzy rules are optimized based on a genetic algorithm. Simulation results show that the above method can provide satisfied robustness, smooth commands and rapid convergence of the fuzzy rules.
Keywords
aircraft control; control system synthesis; fuzzy logic; genetic algorithms; nonlinear control systems; dynamic inverse control law; dynamic inverse controller design; equivalent affine system; equivalent system; fuzzy logic regulars; fuzzy rule optimisation; generic hypersonic vehicle; genetic algorithm; hypersonic vehicles; integrated control law; nonlinear model; Aerodynamics; Aerospace control; Fuzzy logic; Genetic algorithms; Nonlinear dynamical systems; Vehicle dynamics; Vehicles; dynamic inverse; fuzzy logic; genetic algorithm; hypersonic vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Control (ICMC), 2014 International Conference on
Print_ISBN
978-1-4799-2537-7
Type
conf
DOI
10.1109/ICMC.2014.7231595
Filename
7231595
Link To Document