• Electronics Optics & Control
  • Vol. 21, Issue 7, 14 (2014)
GONG Xun and WANG Li
Author Affiliations
  • [in Chinese]
  • show less
    DOI: 10.3969/j.issn.1671-637x.2014.07.004 Cite this Article
    GONG Xun, WANG Li. Attitude Stability Control of the Quad-Rotor Aircraft Based on Fault-Tolerant Technology[J]. Electronics Optics & Control, 2014, 21(7): 14 Copy Citation Text show less
    References

    [1] ZHANG X, PARISINI T, POLYCARPOU M M.Adaptive fault-tolerant control of nonlinear uncertain systems:An information-based diagnostic approach [J] .IEEE Transaction on Automatic Control, 2004, 49(8):1259-1274.

    [2] BOSKOVIC J D, MEHRA R K.Robust fault-tolerant control design for aircraft under state-dependent disturbances [J].AIAA J Guid, Control Dyn, 2005, 28(5):902-917.

    [3] BOSKOVIC J D, MEHRA R K.A Decentralized fault-tolerant control system for accommodation of failures in higher-order flight control actuators [J] .IEEE Transactions on Control System Technology, 2010, 18(5):1103-1115.

    [4] LIN C L, LIU C T.Failure detection and adaptive compensation for fault tolerable flight control systems [J].IEEE Transactions on Industrial Informatics, 2007, 3(4):323-331.

    [5] HABLY A, MARCHAND N.Global stabilization of a four rotor helicopter with bounded inputs [C]//Proceeding of the IEEE/RSJ International Conference on Intelligent Robots and Systems, San Diego, USA, 2007:129-134.

    [6] SHARIFI F, MIRZAEI M, GORDON B W, et al.Fault tolerant control of a quadrotor UAV using sliding mode control [C] //Proceedings of the Conference on Control and Fault Tolerant Systems, Nice France, 2010:239-244.

    [7] RANJBARAN M, KHORASANI K.Generalized fault recovery of an under-actuated quadrotor aerial vehicle [C]//Proceedings of the American Control Conference, Montreal Canada, 2012:2515-2520.

    [8] JIANG H, YU Y, DING X, et al.A fault tolerant control strategy for quadrotor UAVs based on trajectory linearization approach [C]//Proceedings of the IEEE International Conference on Mechatronics and Automation, Chengdu China 2012:1174-1179.

    [9] BOUABDALLAH S, SIEGWART R.Back-stepping and sliding-mode techniques applied to an indoor micro quad-rotor [C]//Proceeding of the IEEE International Conference on Robotics and Automation.Barcelona, Spain, 2005:2247-2252.

    [10] FANTONI L, LOZANO R.Non-linear control for under-actuated mechanical systems [M].Berlin:Springer-Verlag, 2002.

    [11] RAFFO G V, ORTEGA M G, RUBIO F R.Backstepping/nonlinear hinf control for path tracking of a quadrotor unmanned aerial vehicle [C]//Proceeding of the American Control Conference, Washington USA, 2008:3356-3361.

    [12] MAYBECK P S.Application of multiple model adaptive algorithms to reconfigurable flight control [J].Control Dynamic System, 1992(52):291-320.

    [13] GARIMELLA P, YAO B.An adaptive robust framework for model-based state fault detection [C]//Proceeding of the American Control Conference, Minnesota USA, 2006:5692-5697.

    GONG Xun, WANG Li. Attitude Stability Control of the Quad-Rotor Aircraft Based on Fault-Tolerant Technology[J]. Electronics Optics & Control, 2014, 21(7): 14
    Download Citation