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Volume 40 Issue 10
Oct.  2014
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Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(10): 1378-1385.
Wang Fawei, Dong Xinmin, Wang Xiaoping, et al. Fault tolerant control of multi-effectors aircraft using integral sliding model with WPI[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(10): 1378-1385. doi: 10.13700/j.bh.1001-5965.2013.0623(in Chinese)
Citation: Wang Fawei, Dong Xinmin, Wang Xiaoping, et al. Fault tolerant control of multi-effectors aircraft using integral sliding model with WPI[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(10): 1378-1385. doi: 10.13700/j.bh.1001-5965.2013.0623(in Chinese)
shu

Fault tolerant control of multi-effectors aircraft using integral sliding model with WPI

doi: 10.13700/j.bh.1001-5965.2013.0623

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

  • Received Date: 30 Oct 2013
  • Publish Date: 20 Oct 2014
    Abstract
  • An integral sliding model using dynamic adjustment weighted pseudo inverse (WPI) was proposed to fault tolerant control for over-actuated aircraft actuator damaged, which had fault reconstruction error and time delay, position and rate limiting. The instruction restricts module was used to limit saturation control command and instantaneous disturbance. A control allocation scheme using dynamic adjustment WPI was designed to gradually reduce instruction saturation. The control allocation was reconstructed by failure estimate to compensate the aerodynamic loss, which reduced the effects of fault for system stability. An integral siding model control law was designed to ensure system stability with fault reconstruction error and time delay. The simulation results show good track performance, as well as the robust for time delay and tolerant ability for actuator damaged.

     

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