Electronics Optics & Control, Volume. 23, Issue 11, 27(2016)

Dynamic Matrix Control for Fighter Envelope Protection

ZHENG Xin-rui... WU Qing-xian and YE Hui |Show fewer author(s)
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    References(5)

    [2] [2] U.S.Department of Transportation Federal Aviation Administration.Simulation and flight test assessment of safety benefits and certification aspects of advanced flight control systems[R].Springfield: U.S.Public Through the National Technical Information Service(NTIS), 2003.

    [3] [3] HORN J F, CALISE A J, PRASAD J V R.Flight envelope limit detection and avoidance for rotorcraft[J].Journal of the American Helicopter Society, 2002, 47(4): 253-262.

    [5] [5] PRASAD J V R, YAVRUCUK I, UNNIKRISHNAN S.Adaptive limit prediction and avoidance for rotorcraft[C]//Proceedings of the 28th European Rotorcraft Forum, Royal Aeronautical Society, London, 2002: 881-887.

    [6] [6] STEINBERG M L.A comparison of intelligent, adaptive, and nonlinear flight control laws[C]//AIAA Gui-dance, Navi-gation, and Control Conference and Exhibit, Portland, 1999: 9-11.

    [7] [7] MALINOWSKI A, ZURADA J M, LILLY J H.Inverse control of nonlinear system using neural network observer and inverse mapping approach [C]//IEEE International Conference on Neural Networks, 1995: 2513-2518.

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    ZHENG Xin-rui, WU Qing-xian, YE Hui. Dynamic Matrix Control for Fighter Envelope Protection[J]. Electronics Optics & Control, 2016, 23(11): 27

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    Paper Information

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    Received: Oct. 9, 2015

    Accepted: --

    Published Online: Nov. 30, 2016

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2016.11.007

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