UAV Flight Control System Based on an Intelligent BEL Algorithm
Author(s) -
Pu Huangzhong,
Ziyang Zhen,
Ju Jiang,
Daobo Wang
Publication year - 2013
Publication title -
international journal of advanced robotic systems
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.394
H-Index - 46
eISSN - 1729-8814
pISSN - 1729-8806
DOI - 10.5772/53746
Subject(s) - rudder , aileron , computer science , control system , elevator , adaptability , robustness (evolution) , intelligent control , control theory (sociology) , controller (irrigation) , control (management) , control engineering , simulation , artificial intelligence , aerodynamics , engineering , chemistry , electrical engineering , biology , aerospace engineering , ecology , agronomy , biochemistry , structural engineering , marine engineering , gene
A novel intelligent control strategy based on a brain emotional learning (BEL) algorithm is investigated in the application of the attitude control of a small unmanned aerial vehicle (UAV) in this study. The BEL model imitates the emotional learning process in the amygdala-orbitofrontal (A-O) system of mammalian brains. Here it is used to develop the flight control system of the UAV. The control laws of elevator, aileron and rudder manipulators adopt the forms of traditional flight control laws, and three BEL models are used in above three control loops, to on-line regulate the control gains of each controller. Obviously, a BEL intelligent control system is self-learning and self-adaptive, which is important for UAVs when flight conditions change, while traditional flight control systems remain unchanged after design. In simulation, the UAV is on a flat flight and suddenly a wind disturbs it making it depart from the equilibrium state. In order to make the UAV recover to the original equilibrium state, the BEL intelligent control system is adopted. The simulation results illustrate that the BEL-based intelligent flight control system has characteristics of better adaptability and stronger robustness, when compared with the traditional flight control system
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