Liu Jiarun, Shen Gongzhang. Attitude control based on inverse dynamics and online parameter identification[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(02): 111-115. (in Chinese)
Citation: Xi Haijiao, Zhang Xiaolin. Identification of coaxial helicopter dynamic system with elman neural networks[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(7): 861-864. (in Chinese)

Identification of coaxial helicopter dynamic system with elman neural networks

  • Received Date: 13 Sep 2007
  • Publish Date: 31 Jul 2008
  • A modified elman neural network according to the dynamic & kinematic equations of helicopters was established, the training algorithms for the neural networks(NN) was derived, and the training steps and their realizations were provided. From the telemetry data collection of real trial flights of a type of helicopter, the data of typical flying attitudes were exploited to train the NN and calculate the elements of associated weighted matrix, thus the NN for dynamic analysis against the helicopter was obtained. To illustrate the NN effeteness, the vertical operation response in the constant velocity forward flying attitude was simulated, comparing simulation results with real trial flight data shows that the NN basically reflects the real dynamic behavior of the helicopter.

     

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