Electronics Optics & Control, Volume. 20, Issue 3, 44(2013)

Attitude Decoupling Control for Quadrotor Aircraft Based on Active Disturbance Rejection Control Technique

LI Jie... QI Xiaohui and HAN Shuaitao |Show fewer author(s)
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    References(10)

    [1] [1] XU Lifang JIANG Shouda.Research of intelligence control for flying atltitude of four rotors flyer[C]//International Conference on Artificial Intelligence and Computational Intelligence 2010:294-298.

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    [3] [3] FUJIMOTO K YOKOYAMA M TANAB Y.I&I-based adaptive control of a four-rotor mini-helicopter[C]//The 36th Annual Conference on IEEE Industrial Electronics Society 2010:144-149.

    [4] [4] LIU Huanye LI Jian YAO Jianguo et al.Backstepping based adaptive control for a mini rotorcraft with four rotors[C]//The second International Conference on Computer Modeling and Simulation 2010:472-476.

    [5] [5] MCKERROW P.Modelling the draganflyer four-rotor helicopter[C]//Proceedings of the 2004 IEEE International Conference on Robotics and Automation April 26-May 1 2004:3596-3601.

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    [7] [7] RAFFO G V ORTRGA M G.An integral predictive/nonlinear H∞control structure for a quadrotor helicopter[J].Automatica 2010 46:29-39.

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    CLP Journals

    [1] WU Yuewen, ZHENG Bochao, LI Hui. Attitude Controller for Quadrotor via Active Disturbance Rejection Control and Sliding Mode Control[J]. Electronics Optics & Control, 2022, 29(1): 93

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    LI Jie, QI Xiaohui, HAN Shuaitao. Attitude Decoupling Control for Quadrotor Aircraft Based on Active Disturbance Rejection Control Technique[J]. Electronics Optics & Control, 2013, 20(3): 44

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    Paper Information

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    Received: Feb. 19, 2012

    Accepted: --

    Published Online: Mar. 27, 2013

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2013.03.010

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