Systems Engineering and Electronics

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Adaptive tracking control of multi-effector aircraft with actuator nonlinearity

LIU Zongcheng1, CHEN Yong1, DONG Xinmin1, XUE Jianping1, CHENG Jianfeng2, WANG Zutong3   

  1. 1. College of Aeronautics and Astronautics Engineering, Air Force Engineering University, Xi’an 710038, China;
    2. Department of Train Theory, Air Force Xi’an Flight College, Xi’an 710306, China;
    3. Department of Equipment Command, Equipment College, Beijing 101416, China
  • Online:2017-01-20 Published:2010-01-03

Abstract:

A robust adaptive neural network control method based on control allocation is proposed to solve the difficult problem of the tracking control of multi-effector aircraft with actuator nonlinearity. A control allocation equation is developed for multi-effector aircraft with actuator nonlinearity. An adaptive neural network is designed to compensate the nonlinear system uncertainty, and a robust term is introduced to attenuate the effects of external disturbance and system errors. From Lyapunov stability theorem, it is proved that all the signals in the closed-loop system are bounded, and the tracking error can asymptotically converge to zero. Simulation results are presented to demonstrate the effectiveness of this method.

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