Volume 29 Issue 4
Apr.  2014
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YANG Zheng-shan, QIU Xiao-jie, ZHUANG Xi-ming, HUANG Jin-quan. Aero-engine fault-tolerant control based on mode switch[J]. Journal of Aerospace Power, 2014, 29(4): 953-964. doi: 10.13224/j.cnki.jasp.2014.04.028
Citation: YANG Zheng-shan, QIU Xiao-jie, ZHUANG Xi-ming, HUANG Jin-quan. Aero-engine fault-tolerant control based on mode switch[J]. Journal of Aerospace Power, 2014, 29(4): 953-964. doi: 10.13224/j.cnki.jasp.2014.04.028

Aero-engine fault-tolerant control based on mode switch

doi: 10.13224/j.cnki.jasp.2014.04.028
  • Received Date: 2013-02-25
  • Publish Date: 2014-04-28
  • By combining aero-engine control and fault diagnoses methods, the aero-engine fault-tolerant control system based on control mode switch was designed, including task-level mode and engine-level mode. In case of failure of the engine components, the task-level mode could change the control strategies and modes to recover or reduce the aero-engine performance. In case of failure of a control loop, the control strategies were switched to other fault-tolerant control loops according to fault conditions, so as to ensure that the aero-engine continues to work normally. Numerical simulation result shows, the designed fault-tolerant control system can recover the aero-engine performance in 100% in case of failure of the components in the process of steady state or accelerated. And the designed fault-tolerant control system can switch to the fan speed control loop smoothly in 3 seconds in case of failure of the compressor speed control loop.

     

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