Optics and Precision Engineering, Volume. 20, Issue 11, 2450(2012)

Hex-Rotor aircraft and its autonomous flight control system

GONG Xun1,*... BAI Yue2, ZHAO Chang-jun2, GAO Qing-jia2, PENG Cheng1 and TIAN Yan-tao1 |Show fewer author(s)
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  • 2[in Chinese]
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    References(12)

    [1] [1] CASTILLO P, LOZANO R, DZUL A. Stabilization of a mini rotorcraft with four rotors[J]. IEEE Control Systems Magazine, 2005: 45-55.

    [2] [2] ZHANG R, QUAN Q, CAI K Y. Attitude control of a quadrotor aircraft subject to a class of time-varying disturbances[J]. IET Control Theory Appl., 2011, 5(9): 1140-1146.

    [3] [3] DAS A, SUBBARAO K, LEWIS F. Dynamic inversion with zero-dynamics stabilization for quadrotor control[J]. IET Control Theory Appl., 2009. 3(3): 303-314.

    [4] [4] ZUO Z. Trajectory tracking control design with command-filtered compensation for a quadrotor[J]. IET Control Theory Appl., 2010.4(11): 2343-2355.

    [5] [5] ZAIRI S, HAZRY D. Adaptive neural controller implementation in autonomous mini aircraft quadrotor (AMAC-Q) for attitude control stabilization[C]. Proceedings of 2011 IEEE 7th International Colloquium on Signal Proceeding and its Applications, Penang, Malaysia, 2011: 84-89.

    [6] [6] CHEN X J, LI D, XU Z J, et al.. Robust control of quadrotor MAV using self-organizing interval type-II fuzzy neural networks (SOIT-IIFNNs) controller[J]. International Journal of Intelligent Computing and Cybernetics, 2011, 4(3): 397-412.

    [8] [8] NIJMEIJER H, VAN DER SHAFT A J. Nonlinear Dynamic Control Systems[M]. Springer Verlag, 1990.

    [9] [9] FAEELL J A, POLYCARPOU M, DONG W J. Command filtered backstepping[J]. IEEE Transactions on Automatic Control, 2009, 54(6): 1391-1395.

    [10] [10] HAN J Q. From PID technique to “active disturbances rejection control” method[J]. Control Engineering of China, 2002, 9(3): 13-18.(in Chinese)

    CLP Journals

    [1] XU Dong-fu, BAI Yue, GONG Xun, WU Zi-yi, XU Zhi-jun. Correction of 3-axis magnetic compass in multi-rotor UAV under variable control amounts[J]. Optics and Precision Engineering, 2016, 24(8): 1940

    [2] GAO Qing-jia, BAI Yue, SUN Qiang, ZHAO Zhu, ZHAO Chang-jun, GONG Xun. Design and aerodynamic simulation of low Reynolds number rotor airfoil[J]. Optics and Precision Engineering, 2015, 23(2): 511

    [3] ZHANG Xin3, BAI Yue, ZHAO Chang-jun, WANG Ri-jun, GONG Xun, XU Zhi-jun. Improved adaptive extended Kalman algorithm for attitude estimation of multi-rotor UAV[J]. Optics and Precision Engineering, 2014, 22(12): 3384

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    GONG Xun, BAI Yue, ZHAO Chang-jun, GAO Qing-jia, PENG Cheng, TIAN Yan-tao. Hex-Rotor aircraft and its autonomous flight control system[J]. Optics and Precision Engineering, 2012, 20(11): 2450

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    Paper Information

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    Received: May. 21, 2012

    Accepted: --

    Published Online: Nov. 28, 2012

    The Author Email: Xun GONG (as1123@163.com)

    DOI:10.3788/ope.20122011.2450

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