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

被引：0
作者：
Dong W. [1 ]
Tong Y. [2 ]
Zhu P. [2 ,3 ]
Guo J. [4 ]
机构：
[1] Aeronautics Engineering College, Air Force Engineering University, Xi'an
[2] Graduate College, Air Force Engineering University, Xi'an
[3] Naval Aviation University, Huludao
[4] Avionics Department, State-Owned Wuhu Machinery Factory, Wuhu
来源：
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics | 2020年 / 46卷 / 05期
关键词：
Extended state observer; Fault-tolerant control; Multiple faults; Neural network; Transport aircraft;
D O I：
10.13700/j.bh.1001-5965.2019.0346
中图分类号：
学科分类号：
摘要：
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. © 2020, Editorial Board of JBUAA. All right reserved.
引用
收藏
页码：1005 / 1017
页数：12
相关论文
共 22 条
  • [1] Dong Q., Zong Q., Zhang C.F., Et al., Intelligent adaptive control for the large aircraft based on the disturbance compensation under the influence of strong interferences, Scientia Sinica Technologica, 48, 3, pp. 248-263, (2018)
  • [2] Tang X., Tao G., Joshi S.M., Adaptive actuator failure compensation for nonlinear MIMO systems with an aircraft control application, Automatica, 43, 11, pp. 1869-1883, (2007)
  • [3] Alwi H., Edwards C., Fault tolerant control using sliding modes with on-line control allocation, Automatica, 44, 7, pp. 1859-1866, (2008)
  • [4] Chen Y., Dong X.M., Xue J.P., Et al., Adaptive reconfigurable control allocation for over-actuated actuator failures, Journal of Applied Sciences, 29, 5, pp. 537-544, (2011)
  • [5] Huang Y.H., Qi R.Y., Jiang B., Et al., Adaptive failure compensation design for hypersonic vehicles based on dynamic surface backstepping control, Journal of University of Science and Technology of China, 42, 9, pp. 768-774, (2012)
  • [6] Ma J., Ni S.H., Xie W.J., Et al., L1 fault tolerant control for aircraft actuator fault with matched and unmatched uncertainties, Control and Decision, 32, 6, pp. 967-975, (2017)
  • [7] Zhang S.J., Shuang W.F., Li Z.Q., Nonlinear adaptive failure compensation control for flying wing aircraft, Control and Decision, 35, 8, pp. 160-167, (2018)
  • [8] Espinoza-Trejo D.R., Campos-Delgado D.U., Active fault tolerant scheme for variable speed drives under actuator and sensor faults, IEEE International Conference on Control Applications, (2008)
  • [9] Li H., Gao H., Shi P., Et al., Fault-tolerant control of Markovian jump stochastic systems via the augmented sliding mode observer approach, Automatica, 50, 7, pp. 1825-1834, (2014)
  • [10] Du Y.L., Li Y.C., Decentralized active fault-tolerant control for reconfigurable manipulator with simultaneous faults, Journal of Central South University(Science and Technology), 45, 3, pp. 727-733, (2014)
123