Volume 22 Issue 5
May  2007
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Article Navigation >  Journal of Aerospace Power  > 2007  >  22(5): 829-832
LI Sheng-quan, YANG Zheng-shan, SUN Jian-guo. Investigation of state feedback control based on internal model principle for an turbo-shaft Engine[J]. Journal of Aerospace Power, 2007, 22(5): 829-832.
Citation: LI Sheng-quan, YANG Zheng-shan, SUN Jian-guo. Investigation of state feedback control based on internal model principle for an turbo-shaft Engine[J]. Journal of Aerospace Power, 2007, 22(5): 829-832.
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Investigation of state feedback control based on internal model principle for an turbo-shaft Engine

  • 1.

    College of Energy and Power Engineering, Nanjing University of Aeronauticsand Astronautics, Nanjing 210016, China

  • 2.

    Aviation Motor Control System Institute, Wuxi 214063, China

  • Received Date: 2006-04-05
  • Rev Recd Date: 2007-03-09
  • Publish Date: 2007-05-28
    Abstract
  • A turbo-shaft engine FADEC system is subjected to the state feedback control mode.Based on the internal principle,a servo-compensator was introduced such that the control system could present strong robustness,and also eliminate steady state errors when tracking with commands.According to performance index,a states feedback controller was also designed to improve the performance of the control system.As compared with PID control method,the test results show an outstanding performance of the control system.

     

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    • References(6)
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