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Volume 42 Issue 9
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Journal of Beijing University of Aeronautics and Astronautics  > 2016  >  42(9): 1864-1873.
LIU Haidong, BAO Weimin, LI Huifeng, et al. Attitude control method within finite time globally for hypersonic vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(9): 1864-1873. doi: 10.13700/j.bh.1001-5965.2015.0547(in Chinese)
Citation: LIU Haidong, BAO Weimin, LI Huifeng, et al. Attitude control method within finite time globally for hypersonic vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(9): 1864-1873. doi: 10.13700/j.bh.1001-5965.2015.0547(in Chinese)
shu

Attitude control method within finite time globally for hypersonic vehicles

doi: 10.13700/j.bh.1001-5965.2015.0547
  • 1.

    School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • 2. Science and Technology on Space Physics Laboratory, Beijng 100076, China

  • 3. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China

  • Received Date: 26 Aug 2015
  • Publish Date: 20 Sep 2016
    Abstract
  • Taking six degrees of freedom model of a generic hypersonic vehicle as the research object, this paper proposes a terminal sliding mode attitude control method which can converge to the equilibrium point within finite time globally. In the design of the controller, dynamic inversion is applied to deal with strong couplings among pitch angle, yaw angle and roll angle. In the case of considering the model uncertainties and external disturbances, the terminal sliding mode variable structure control method is used to guarantee the robustness of the system. In addition, by improving the traditional exponential approach law, the control command can be tracked within finite time globally. Based on the Lyapunov stability theory, it is proved that the finite time convergence in both reaching and sliding phases can be achieved. Finally, simulation results demonstrate that the proposed attitude control method is efficient.

     

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