• Electronics Optics & Control
  • Vol. 28, Issue 3, 46 (2021)
ZHANG Jiawen1, SHI Jinguang1, LIU Jiajia2, and XU Donghui2
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2021.03.009 Cite this Article
    ZHANG Jiawen, SHI Jinguang, LIU Jiajia, XU Donghui. Sliding Mode Guidance Law of Means Clustering Neural Network with Falling Angle Constraint[J]. Electronics Optics & Control, 2021, 28(3): 46 Copy Citation Text show less
    References

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    [9] SONG J M, ZHANG T Q.Passive homing missiles variable structure proportional navigation with terminal angular constraint[J].Chinese Journal of Aeronautics, 2001, 14(2): 83-87.

    [10] QIN T, CHEN W C, XING X L.A method for precision missile guidance with impact attitude angle constraint [J].Journal of Astronautics, 2012, 33(5): 570-576.

    [13] KUMAR S R, RAO S, GHOSE D.Nonsingular terminal sliding mode guidance with impact angle constraints[J].Journal of Guidance, Control and Dynamics, 2014, 22(5): 1114-1130.

    [14] ZHAO Y, SHENG Y Z, LIU X D.Sliding mode control based guidance law with impact angle constraint[J].Chinese Journal of Aeronautics, 2014, 27(1): 145-152.

    ZHANG Jiawen, SHI Jinguang, LIU Jiajia, XU Donghui. Sliding Mode Guidance Law of Means Clustering Neural Network with Falling Angle Constraint[J]. Electronics Optics & Control, 2021, 28(3): 46
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