• Electronics Optics & Control
  • Vol. 29, Issue 7, 1 (2022)
HUA Wenhua1 and ZHANG Jinpeng1、2
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2022.07.001 Cite this Article
    HUA Wenhua, ZHANG Jinpeng. Adaptive Sliding Mode Guidance Law of Flight Velocity Adjustable Missiles[J]. Electronics Optics & Control, 2022, 29(7): 1 Copy Citation Text show less
    References

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    [5] BABA Y, TAKEHIRA T, TAKANO H.New guidance law for a missile with varying velocity[C]//Proceedings of the AIAA Guidance, Navigation, and Control Conference.Scottsdale:AIAA, 1994:207-215.

    [6] CHO H, RYOO C K, TAHK M J.Closed-form optimal gui-dance law for missiles of time-varying velocity[J].Journal of Guidance, Control, and Dynamics, 1996, 19(5):1017-1022.

    [7] TEKIN R, ERER K S, HOLZAPFEL F.Adaptive impact time control via look-angle shaping under varying velocity[J].Journal of Guidance, Control, and Dynamics, 2017, 40(12):3247-3255.

    [8] SHINAR J, SHIMA T.Nonorthodox guidance law development approach for intercepting maneuvering targets[J].Journal of Guidance, Control, and Dynamics, 2002, 25(4):658-666.

    [11] MISHRA A, SINHA N K.Design of adaptive sliding mode control for uncertain thrust vectored airship[C]//AIAA Guidance, Navigation, and Control Conference.Kissimmee: AIAA, 2018:AIAA 2018-1129.

    [13] YANG J, STOLL E.Adaptive sliding mode control for spacecraft proximity operations based on dual quaternions[J].Journal of Guidance, Control, and Dynamics, 2019, 42(11):2356-2368.

    HUA Wenhua, ZHANG Jinpeng. Adaptive Sliding Mode Guidance Law of Flight Velocity Adjustable Missiles[J]. Electronics Optics & Control, 2022, 29(7): 1
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