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Volume 42 Issue 11
Nov.  2016
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Journal of Beijing University of Aeronautics and Astronautics  > 2016  >  42(11): 2454-2465.
LIN Qing, CAI Zhihao, YAN Kun, et al. Influence of pitch manipulation modes on controllability and stability of autogyro[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(11): 2454-2465. doi: 10.13700/j.bh.1001-5965.2015.0776(in Chinese)
Citation: LIN Qing, CAI Zhihao, YAN Kun, et al. Influence of pitch manipulation modes on controllability and stability of autogyro[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(11): 2454-2465. doi: 10.13700/j.bh.1001-5965.2015.0776(in Chinese)
shu

Influence of pitch manipulation modes on controllability and stability of autogyro

doi: 10.13700/j.bh.1001-5965.2015.0776
  • 1.

    School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • 2. Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 25 Nov 2015
  • Rev Recd Date: 27 Jan 2016
  • Publish Date: 20 Nov 2016
    Abstract
  • To study the influence of two manipulation modes on flight dynamics characteristics of autogyro, an example autogyro UAV was chosen and modeled based on closed-form blade element method. Then the differences of the two modes in trim results, stability and handling characteristics were analyzed in the whole speed envelope. The results indicate that each manipulation mode has its advantages and disadvantages:for the rotor manipulation mode, the trim pitch angle has little change and the phugoid mode is stable, but the spiral mode is unstable in the whole envelope. For the elevator manipulation mode, the spiral mode is stable at relatively high speed and the attainable pitch moment is larger, but the trim angle of attack is negative at high speed and the speed static stability is negative. Then two prototype autogyro UAVs were assembled and flight-tested for the two manipulation modes respectively. The autorotation of the main rotor during the whole flight were analyzed. Attitude control laws were designed and flight-tested for the two prototype UAVs, which both achieve attitude tracking relatively well. Finally, the model of the autogyro UAV was validated with the flight test data.

     

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