• Electronics Optics & Control
  • Vol. 23, Issue 7, 55 (2016)
WANG Da-wei1 and GAO Xi-feng2
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2016.07.012 Cite this Article
    WANG Da-wei, GAO Xi-feng. Design of Sliding Mode Trajectory Tracking Controllers for Quadrotor Aircraft[J]. Electronics Optics & Control, 2016, 23(7): 55 Copy Citation Text show less
    References

    [1] PETER L, CHEN Y N, ALBER Y, et al.A review of rotorcraft Unmanned Aerial Vehicle(UAV) developments and applications in civil engineering[J].Smart Structures and Systems, 2013, 13(6): 1065-1094.

    [7] XU R, OZGUNER U. Sliding mode control of a class of underactuated systems[J]. Automatica, 2008, 44(1): 233-241. XIONG J J, ZHENG E H. Position and attitude tracking control for a quadrotor UAV[J]. ISA Transactions, 2014, 53(3): 725-731.

    [10] GUIHERNE V, MANUEL G, FRANCISCO R. Backstepping/H∞ control for path tracking of a quadrotor unman-ned aerial vehicle[C]//American Control Conference, Seattle, 2008: 3356-3361.

    [11] GUIHERME V, MANUEL G, FRANCISCO R. An integral predictive/nonlinear H∞ control structure for quadrotor helicopter[J]. Automatica, 2010, 46(1): 29-39.

    WANG Da-wei, GAO Xi-feng. Design of Sliding Mode Trajectory Tracking Controllers for Quadrotor Aircraft[J]. Electronics Optics & Control, 2016, 23(7): 55
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