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Volume 38 Issue 9
Sep.  2012
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Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  (9): 1194-1199.
Wang Lijing, Yuan Xiugan, Li Yinxia, et al. Analysis on reach envelop of pilot in cockpit[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(01): 41-44. (in Chinese)
Citation: Li Jingjing, Ren Zhang, Shen Zhenet al. Design of decentralized robust attitude controller for hypersonic sliding vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (9): 1194-1199. (in Chinese)
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Design of decentralized robust attitude controller for hypersonic sliding vehicles

  • Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 06 May 2011
  • Publish Date: 30 Sep 2012
    Abstract
  • Based on the mission and aerodynamic features of hypersonic sliding vehicles, the control-oriented model was built by taking first-order actuator dynamics into account. The decentralized robust attitude controller for re-entry flight incorporated the idea of decentralized control and sliding mode control was designed. And the decentralized robust sliding surfaces were designed using Tornambe control technique to ensure good tracking performance in sliding mode in the presence of coupling and unmatched uncertainties. The second order sliding mode control law was synthesized using modified sub-optimal control method in which the on-line estimate of equivalent control reduced chattering. Finally, a six-degree-of-freedom simulation in Simulink for a conceptual hypersonic sliding vehicle was performed, the robust tracking of guidance command is guaranteed despite of large parameter perturbations.

     

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    • References(9)
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