Volume 28 Issue 7
Jul.  2013
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ZHANG Hai-bo, YE Fei, LI Yong-jin, CHEN Guo-qiang. Semi-physical simulation on integrated helicopter/engine control system[J]. Journal of Aerospace Power, 2013, 28(7): 1650-1658.
Citation: ZHANG Hai-bo, YE Fei, LI Yong-jin, CHEN Guo-qiang. Semi-physical simulation on integrated helicopter/engine control system[J]. Journal of Aerospace Power, 2013, 28(7): 1650-1658.

Semi-physical simulation on integrated helicopter/engine control system

  • Received Date: 2012-07-15
  • Publish Date: 2013-07-28
  • Based on the simulation platform of integrated helicopter/engine system control,semi-physical simulations were carried out for integrated helicopter/engine model and integrated control algorithm.The core part of anti-disturbance control of the integrated system adopted a novel algorithm of cascade proportional integration differential(PID)+torque feed forward+collective compensation,and the optimization control was multi-mode real-time optimization based on the simplified engine adaptive system model.The simulation tests show that the established integrated helicopter/engine model can simulate the engine's total process from start to idling,then to helicopter flying,and the droop and overshoot of the power turbine is within 4% in the whole process.The engine's dynamic and static quality meets the requirements of helicopter flight control in different flight conditions.The semi-physical simulation results of the integrated system multi-mode optimization were validated.The established semi-physical simulation platform of integrated helicopter/engine control system is valuable for engineering applications.

     

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