• Electronics Optics & Control
  • Vol. 24, Issue 12, 22 (2017)
LIU Rong1,2, XIAO Ying-feng3, LIANG Jin4, and YAO Cheng-kang4
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
  • 4[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2017.12.005 Cite this Article
    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 Copy Citation Text show less
    References

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

    [8] LIU T H, LEE Y C, CHANG Y H. Adaptive controller design for linear motor control system[J]. IEEE Transactions on Aerospace and Electronic Systems, 2004, 40(2): 601-616.

    [10] KAZANTZIS N, KRAVARIS C, TSERONIS C, et al. Optimal controller tuning for nonlinear process[J]. IFAC Proceedings Volumes, 2002, 35(1): 453-458.

    [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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