• Electronics Optics & Control
  • Vol. 20, Issue 6, 12 (2013)
GAO Xiaoxiang, ZHOU Deyun, and ZHOU Canhui
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2013.06.004 Cite this Article
    GAO Xiaoxiang, ZHOU Deyun, ZHOU Canhui. An Improved Three-Dimensional Variable Structure Guidance Law for Air-to-Air Missiles[J]. Electronics Optics & Control, 2013, 20(6): 12 Copy Citation Text show less
    References

    [4] LEE J IJEON I STAHK M J.Guidance law to control impact time and angle[J].IEEE Transactions on Aerospace and Electronic Systems200743(1):301-309.

    [6] ZHOU DiMU ChundiLING Qianget al.Optimal sli-ding-mode guidance of a homing-missile[C]//Proceeding of the 38th Conference on Decision and Control Phoenix USA19-9912:5131-5136.

    GAO Xiaoxiang, ZHOU Deyun, ZHOU Canhui. An Improved Three-Dimensional Variable Structure Guidance Law for Air-to-Air Missiles[J]. Electronics Optics & Control, 2013, 20(6): 12
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