• Electronics Optics & Control
  • Vol. 22, Issue 12, 59 (2015)
XING Jin-he, WANG Xue-mei, XU Zhe, and ZHENG Gang
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2015.12.012 Cite this Article
    XING Jin-he, WANG Xue-mei, XU Zhe, ZHENG Gang. Variable Structure Guidance Law Based on Genetic Algorithm[J]. Electronics Optics & Control, 2015, 22(12): 59 Copy Citation Text show less
    References

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    [3] ZHOU D,MU C,LING Q,et al.Optimal sliding-mode guidance of a homing-missile[J].Chinese Journal of Aeronautics,1999,12(4):236-241.

    [4] ZHOU D,MU C,XU W L.Adaptive sliding-mode guidance of a homing missile[J].Journal of Guidance,Control and Dynamics,1999,22(4):589-594.

    [5] WANG Z,JIA X H,YAN J.Study on the ENDGAME sliding-mode guidance law of air-to-air missile[J].Aero Weaponry,2005(2):3-6.

    [6] LI Y.Study on variable structure terminal guidance law and stability of space interception[D].Harbin:Harbin Institute of Technology,2011.

    [7] YUAN L Y.Nonlinear guidance law for interception of maneuvering target[D].Harbin:Harbin Institute of Technology,2008.

    XING Jin-he, WANG Xue-mei, XU Zhe, ZHENG Gang. Variable Structure Guidance Law Based on Genetic Algorithm[J]. Electronics Optics & Control, 2015, 22(12): 59
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