Volume 29 Issue 4
Apr.  2014
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FU Qiang, FAN Ding, PENG Kai. Active fault tolerant controller designo of aero-engine main fuel metering valve[J]. Journal of Aerospace Power, 2014, 29(4): 973-979. doi: 10.13224/j.cnki.jasp.2014.04.030
Citation: FU Qiang, FAN Ding, PENG Kai. Active fault tolerant controller designo of aero-engine main fuel metering valve[J]. Journal of Aerospace Power, 2014, 29(4): 973-979. doi: 10.13224/j.cnki.jasp.2014.04.030

Active fault tolerant controller designo of aero-engine main fuel metering valve

doi: 10.13224/j.cnki.jasp.2014.04.030
  • Received Date: 2013-03-22
  • Publish Date: 2014-04-28
  • In case of failure of aero-engine main fuel metering valve actuator, the output of system will have the jumping problem, and will not track the system to the desired output. The model reference adaptive design method of active fault tolerant controller will solve this problem. Firstly,the actuator faults have been described mathematically. Secondly, the system nominal model was selected as the reference model, and the output error minimization selected as optimization objective; then lyapunov stability theory was used to search for a suitable adaptive law, and an adaptive fault tolerant controller was designed. Finally, the numerical simulation of different fault diagnosis of engine operating points was conducted. The simulation results show that, in case of jumping fault and blocking of the main fuel metering valve, adaptive fault tolerant controller can automatically adjust the parameters, making the system output track the model output, and the final tracking error is nearly zero.

     

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