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Volume 46 Issue 5
May  2020
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Journal of Beijing University of Aeronautics and Astronautics  > 2020  >  46(5): 1005-1017.
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Citation: DONG Wenhan, TONG Yingyi, ZHU Peng, et al. Multiple-fault fault-tolerant control of transport aircraft based on extended state observer[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(5): 1005-1017. doi: 10.13700/j.bh.1001-5965.2019.0346(in Chinese)
shu

Multiple-fault fault-tolerant control of transport aircraft based on extended state observer

doi: 10.13700/j.bh.1001-5965.2019.0346
  • 1.

    Aeronautics Engineering College, Air Force Engineering University, Xi'an 710038, China

  • 2.

    Graduate College, Air Force Engineering University, Xi'an 710038, China

  • 3.

    Naval Aviation University, Huludao 125001, China

  • 4.

    Avionics Department, State-Owned Wuhu Machinery Factory, Wuhu 241000, China

Funds:

Aeronautical Science Foundation of China 20171396

More Information
  • Corresponding author: DONG Wenhan, E-mail:dongwenhan@sina.com
  • Received Date: 28 Jun 2019
  • Accepted Date: 15 Oct 2019
  • Publish Date: 20 May 2020
    Abstract

  • To solve the attitude tracking problem of transport aircraft with sensor faults and actuator faults, a backstepping fault-tolerant control method based on extended state observer is proposed. The state observer and controller are designed separately. The extended state observer with neural network is designed to estimate the flight states, sensor faults and actuator faults simultaneously. On this basis, the flight states are replaced by the estimates, the control law of attitude tracking control is designed based on backstepping control technique, and the command filter is also introduced into the fault-tolerant controller which can improve the control performance.The final bounded convergence of closed-loop system tracking errors is derived and proved using Lyapunov stability analysis. The simulation results show that the proposed method is effective and can solve the attitude angle tracking problem of transport aircraft in the presence of sensor faults and actuator faults.

     

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