Non-affine Nonlinear Flight Control System Based on Robust Adaptive Fault-tolerant Control

نویسندگان

  • Zhou Hong - Cheng
  • Wang Dao - Bo
چکیده

For non-affine nonlinear flight control systems, a non-affine nonlinear robust fault tolerance control method is proposed. Here, the fault tolerance control framework is used, and on this basis, observer-based auxiliary system is designed to implicit fault parameters and disturbances information. Then reconfigurable controller is designed using the dynamic of observer-based auxiliary system, which can realize non-affine nonlinear systems robust adaptive fault-tolerant. Simulation results show the effectiveness of the proposed method. Copyright © 2014 IFSA Publishing, S. L.

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تاریخ انتشار 2014