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Volume 40 Issue 2
Feb.  2014
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Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(2): 177-182.
Wu Zhendong, Wang Qing, Dong Chaoyanget al. Robust H∞ control for hypersonic vehicles under asynchronous switching[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(2): 177-182. (in Chinese)
Citation: Wu Zhendong, Wang Qing, Dong Chaoyanget al. Robust H∞ control for hypersonic vehicles under asynchronous switching[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(2): 177-182. (in Chinese)
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Robust H∞ control for hypersonic vehicles under asynchronous switching

  • 1.

    School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • 2. School of Aeronautical Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 16 Apr 2013
  • Publish Date: 20 Feb 2014
    Abstract
  • A new robust H∞ control design method was presented for hypersonic vehicles under asynchronous switching between the controllers and subsystems. A Lyapunov function dependent on switching signal of controllers was constructed, which could effectively counteract the intractable problem of controller design under asynchronous switching. Moreover, employing the average dwell time technique and Lyapunov function method, the globally uniformly asymptotically stable with the H∞ performance index was investigated, and the robust H∞ controllers were designed. Simulation results show that the robust H∞ control system of hypersonic vehicles provides satisfactory command tracking and avoids the state jumping under asynchronous switching with a high containment procedure for the turbulence.

     

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