Electronics Optics & Control, Volume. 21, Issue 9, 58(2014)

Trajectory Control of a UAV During Net Recovery Based on Sliding Mode Control and Optimal Control

LI Ruolan... ZHEN Ziyang and GONG Huajun |Show fewer author(s)
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    References(7)

    [1] [1] PEI J H.Technology development of UAV net recovery system[J].Journal of Nanjing University of Aeronautics and Astronautics200941(s):6-11.

    [2] [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] [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] [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] [5] LIZARRAGA M.Autonomous landing system for a UAV[D].Monterey:Naval Postgraduate School2004.

    [6] [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] [7] LIU J K.MATLAB simulation for sliding mode control[M].Beijing:Tsinghua University Press2005.

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    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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    Paper Information

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    Received: Sep. 10, 2013

    Accepted: --

    Published Online: Sep. 15, 2014

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2014.09.013

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