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Volume 41 Issue 9
Sep.  2015
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Journal of Beijing University of Aeronautics and Astronautics  > 2015  >  41(9): 1749-1757.
HUANG Kangqiang, ZHAO Hui, REN Yang, et al. Standard trajectory guidance for CAV reentry based on fuzzy sliding mode control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(9): 1749-1757. doi: 10.13700/j.bh.1001-5965.2014.0742(in Chinese)
Citation: HUANG Kangqiang, ZHAO Hui, REN Yang, et al. Standard trajectory guidance for CAV reentry based on fuzzy sliding mode control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(9): 1749-1757. doi: 10.13700/j.bh.1001-5965.2014.0742(in Chinese)
shu

Standard trajectory guidance for CAV reentry based on fuzzy sliding mode control

doi: 10.13700/j.bh.1001-5965.2014.0742

  • School of Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an 710038, China

  • Received Date: 28 Nov 2014
  • Publish Date: 20 Sep 2015
    Abstract
  • For the question that the standard trajectory guidance was too sensitive to initial value of state and robustness was worse, a new standard trajectory guidance method based on the fuzzy sliding mode control was proposed. The robustness of sliding mode control was used to improve the adaptive capacity of guidance method, in order to definitely estimate the uncertain factors, the universal approximation property of fuzzy system was used to approach uncertain factors. Through analyzing the determinate principle of membership function combined with the characteristics of reentry process, the longitudinal guidance law was established, the simulation results validate that the master control law combined fuzzy approximation with state feedback is effective. And the lateral guidance law was designed based on the scheme mentioned before. Numerical simulation results show that this method can not only ensure a high precision but also improve the robustness of standard trajectory guidance law, and simplify the calculation process greatly.

     

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