Electronics Optics & Control, Volume. 24, Issue 12, 22(2017)

An Optimal Algorithm of Control Law Access Time for Folding-Wing UAVs

LIU Rong1...2, XIAO Ying-feng3, LIANG Jin4 and YAO Cheng-kang4 |Show fewer author(s)
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  • 1[in Chinese]
  • 2[in Chinese]
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    References(6)

    [3] [3] JACOB J D, SMITH S W. Design limitations of deployable wings for small low altitude UAVs[C]//The 47th AIAA Aerospace Sciences Meeting Including, The New Horizons Forum and Aerospace Exposition, Orlando, Florida, AIAA, 2009, 745: 516-525.

    [4] [4] SNYDER M P, SANDERS B, EASTEP F E, et al. Vibration and flutter characteristics of a folding wing[J]. Journal of Aircaft, 2009, 46(3): 791-799.

    [7] [7] KO S, BITMEAD R R. Optimal control for linear systems with state equality constraints[J]. Automatica, 2007, 43(9): 1573-1582.

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    [11] [11] LI X R, ZHU Y M, WANG J, et al. Optimal linear estimation fusion, Part I: unified fusion rules[J]. IEEE Transactions on Information Theory, 2007, 49(9): 2192-2208.

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    [1] WANG Suzhen, LIU Jianfeng. Multi-model Adaptive Control of Nonlinear Systems Based on Improved BP Neural Network[J]. Electronics Optics & Control, 2021, 28(8): 1

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    LIU Rong, XIAO Ying-feng, LIANG Jin, YAO Cheng-kang. An Optimal Algorithm of Control Law Access Time for Folding-Wing UAVs[J]. Electronics Optics & Control, 2017, 24(12): 22

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    Paper Information

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    Received: Mar. 21, 2017

    Accepted: --

    Published Online: Jan. 22, 2021

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2017.12.005

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