• Electronics Optics & Control
  • Vol. 21, Issue 9, 58 (2014)
LI Ruolan, ZHEN Ziyang, and GONG Huajun
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2014.09.013 Cite this Article
    LI Ruolan, ZHEN Ziyang, GONG Huajun. Trajectory Control of a UAV During Net Recovery Based on Sliding Mode Control and Optimal Control[J]. Electronics Optics & Control, 2014, 21(9): 58 Copy Citation Text show less
    References

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    [2] WEN G LWEN DYIN H Fet al.Dynamic simulation of netrecovery system for unmanned aerial vehicle[J].Journal of Hunan University:Natural Sciences Edition201138(10):34-38.

    [3] URNES J MHESS R K.Integrated flight control systems development — the F/A18A automatic carrier landing system [C]//Guidance and Control Conference GatlinburgTNCollection of Technical PapersUnited States 1983:920-930.

    [4] GAO J J.Situation and development trend of naval shipboard unmanned aerial vehicle[J].Ship Electronic Engineering200424(3):16-19,25.

    [5] LIZARRAGA M.Autonomous landing system for a UAV[D].Monterey:Naval Postgraduate School2004.

    [6] KHANTSIS S.Control system design using evolutionary algorithms for autonomous shipboard recovery of unmanned aerial vehicles[D].Melbourne:Royal Melbourne Institute of Technology2006.

    [7] LIU J K.MATLAB simulation for sliding mode control[M].Beijing:Tsinghua University Press2005.

    LI Ruolan, ZHEN Ziyang, GONG Huajun. Trajectory Control of a UAV During Net Recovery Based on Sliding Mode Control and Optimal Control[J]. Electronics Optics & Control, 2014, 21(9): 58
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