Electronics Optics & Control, Volume. 25, Issue 8, 43(2018)

Longitudinal Control Law Design of Carrier UAV During Carrier Landing

ZAHO Donghong1,2, LI Chuntao1, and ZHANG Xiaowei1
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • show less
    References(3)

    [2] [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] [5] LAVRETSKY E, WISE K A.Robust and adaptive control:with aerospace applications[M].London:Springer, 2013.

    [6] [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.

    Tools

    Get Citation

    Copy Citation Text

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

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Save article for my favorites
    Paper Information

    Category:

    Received: Aug. 31, 2017

    Accepted: --

    Published Online: Jan. 19, 2021

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2018.08.009

    Topics