Electronics Optics & Control, Volume. 25, Issue 4, 87(2018)

Considerations on Structural Modal Coupling in FBW Control Law Design of Civil Aircrafts

LIU Jun... ZHAO Jinghui, KUANG Qun and ZHENG Xiaohui |Show fewer author(s)
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    References(3)

    [4] [4] CHAKRAVARTY A. Inflight evaluation of a modal suppression yaw damper[C]//AIAA Guidance, Navigation and Control Conference, Monterey, California, 1987: 163-169.

    [5] [5] TRAN C B, GOSLIN T J, HO J K, et al. Aircraft fore and aft model suppression system[C]//Proceedings of the 26th Conference on Decision and Control, Los Angeles, 1987: 2337-2440.

    [6] [6] EVERS S D, BERG M C. Simultaneous control-law synthesis of an aircraft yaw-damper and modal suppression system using parameter optimization[C]//Navigation and Control Conference, Washington, AIAA-91-2630, 1991: 287- 297.

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    LIU Jun, ZHAO Jinghui, KUANG Qun, ZHENG Xiaohui. Considerations on Structural Modal Coupling in FBW Control Law Design of Civil Aircrafts[J]. Electronics Optics & Control, 2018, 25(4): 87

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    Paper Information

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    Received: May. 13, 2017

    Accepted: --

    Published Online: Jan. 21, 2021

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2018.04.019

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