• Electronics Optics & Control
  • Vol. 22, Issue 10, 24 (2015)
WANG Yong-chao, ZHANG Sheng-xiu, HU Xiao-xiang, CUI Ya-long, and CAO Li-jia
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2015.10.006 Cite this Article
    WANG Yong-chao, ZHANG Sheng-xiu, HU Xiao-xiang, CUI Ya-long, CAO Li-jia. Adaptive Fuzzy H∞ Control for a Hypersonic Vehicle with Uncertainty Parameters[J]. Electronics Optics & Control, 2015, 22(10): 24 Copy Citation Text show less
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    [1] YU W B,CHEN W C.Guidance scheme for glide range maximization of a hypersonic vehicle[R].AIAA-2011-6714,Reston: AIAA,2011.

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    [9] XU B,SHI Z K,YANG C G,et al.Neural hypersonic flight control via time-scale decomposition with throttle setting constraint[J].Nonlinear Dynamics,2013,73(3): 1849-1861.

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    [11] WANG L X.Fuzzy systems are universal approximators[C]//IEEE International Conference on Fuzzy Systems, San Diego,1992: 1163-1170.

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    WANG Yong-chao, ZHANG Sheng-xiu, HU Xiao-xiang, CUI Ya-long, CAO Li-jia. Adaptive Fuzzy H∞ Control for a Hypersonic Vehicle with Uncertainty Parameters[J]. Electronics Optics & Control, 2015, 22(10): 24
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