• Electronics Optics & Control
  • Vol. 20, Issue 3, 44 (2013)
LI Jie, QI Xiaohui, and HAN Shuaitao
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2013.03.010 Cite this Article
    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 Copy Citation Text show less
    References

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    [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] 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.

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    [6] BENALLEGUE A MOKHTARI A.High-order sliding-mode observer for a quadrotor UAV[J].International Journal of Robust and Nonlinear Control 2008 18:427-440.

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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

    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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