• Electronics Optics & Control
  • Vol. 25, Issue 8, 43 (2018)
ZAHO Donghong1、2, LI Chuntao1, and ZHANG Xiaowei1
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2018.08.009 Cite this Article
    ZAHO Donghong, LI Chuntao, ZHANG Xiaowei. Longitudinal Control Law Design of Carrier UAV During Carrier Landing[J]. Electronics Optics & Control, 2018, 25(8): 43 Copy Citation Text show less
    References

    [2] SINGH L, MIOTTO P, BREGER L.L1 adaptive control design for improved handling of F/A-18 class of aircraft[C]//AIAA Guidance, Navigation, and Control Conference, 2013:1-12.

    [5] LAVRETSKY E, WISE K A.Robust and adaptive control:with aerospace applications[M].London:Springer, 2013.

    [6] URNES J, HESS R, MOOMAW R, et al.Development of the navy H-Dot automatic carrier landing system designed to give improved approach control in air turbulence[C]//Guidance and Control Conference, 1979:451-455.

    ZAHO Donghong, LI Chuntao, ZHANG Xiaowei. Longitudinal Control Law Design of Carrier UAV During Carrier Landing[J]. Electronics Optics & Control, 2018, 25(8): 43
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