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基于联合多观测器的四旋翼直升机故障诊断 被引量:3

Joint Multi-Observer Based Fault Diagnosis for Quadrotor Helicopter
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摘要 针对四旋翼飞行器在发生执行器故障情况下难以进行故障估计的问题,基于增广故障估计观测器和Luenberger故障检测观测器,提出了一种较为新颖的联合多观测器的故障诊断设计方法。该设计方法不仅能够有效地估计单通道执行器故障,解决故障分布阵列不满秩问题下故障估计难的问题,而且拓宽了增广故障估计观测器的适用范围。最后,通过Quanser 3-DOF Hover平台验证了所提算法的可靠性和有效性。 For the quadrotor aircraft in case of actuator failures is difficult to fault estimation problem,a relatively new joint multiple fault diagnosis observers design method is proposed based on the augmented fault estimation observer and the Luenberger fault detection observer.The design method can effectively estimate the single actuator fault,troubleshoot the problem that fault distribution matrix is not full column rank,and widened the application scope of the augmented fault estimation observer.Finally,the proposed algorithm is verified to be reliable and valid on Quanser 3-DOF Hover platform.
出处 《控制工程》 CSCD 北大核心 2012年第S1期222-226,229,共6页 Control Engineering of China
基金 国家自然科学基金(90816023 61074080) 航空科技创新基金(08C52001)
关键词 故障诊断 多观测器 增广故障估计观测器 四旋翼直升机 线性矩阵不等式 fault diagnosis multiple observers augmented fault estimation observer quadrotor linear matrix inequalities
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参考文献11

  • 1张柯,姜斌.基于故障诊断观测器的输出反馈容错控制设计[J].自动化学报,2010,36(2):274-281. 被引量:42
  • 2Magill J,Bachmann M,Rixon G,et al.Dynamic stall control using a model-based observer[].Journal of Air-craft.2003
  • 3W Xie.An Equivalent LMI Representation of Bounded Real Lemma for Continuous-Time Systems[].Journal of Inequalities and Applications.2008
  • 4Wang H,Daley S.Actuator fault diagnosis: An adaptive observer-based technique[].IEEE Transactions on Automatic Control.1996
  • 5Jiang Bin,Wang Jianliang,Soh Yengchai.An adaptive technique for robust diagnosis of faults with independent effect on system out- puts[].International Journal of Control.2002
  • 6Shakernia O,Ma Y,Koo T J,et al.Landing an unmanned air vehicle: vision based motion estimation and nonlinear control[].Asian Journal of Control.1999
  • 7Kazuo Tanaka,Hiroshi Ohtake,Huo O Wang.A Practical Design Approach to Stabilization of a3-DOF RC Helicopter[].IEEE Transactions on Control Systems Technology.2004
  • 8M.Bodson,and J.E.Groszkiewicz.“Multivariable adaptive algorithms for reconfigurable flight control,”[].IEEE Transactions on Control Systems Technology.1997
  • 9Dauglas R K,Speyer J L.Robust fault detection filter design[].Journal of Guidance Control Dynamics.1996
  • 10Chen R H,Speyer J L.Sensor and actuator fault recon-struction[].Journal of Guidance Control and Dynamics.2004

二级参考文献15

  • 1陈茂银,周东华.一类非线性系统的故障诊断[J].自动化学报,2004,30(6):1011-1016. 被引量:10
  • 2Chen J, Patton R J. Robust Model-Based Fault Diagnosis for Dynamic Systems. Boston: Kluwer Academic Publishers, 1999.
  • 3Blanke M, Kinnaert M, Lunze J, Staroswiecki M. Diagnosis and Fault-Tolerant Control. Berlin: Springer-Verlag, 2006.
  • 4Magill J, Bachmann M, Rixon G, McManus K. Dynamic stall control using a model-based observer. Journal of Aircraft, 2003, 40(2): 355-362.
  • 5Zhang Y W, Qin S J. Adaptive actuator/component fault compensation for nonlinear systems. American Institute of Chemical Engineers Journal, 2008, 54(9): 2404-2412.
  • 6Wang H, Daley S. Actuator fault diagnosis: an adaptive observer-based technique. IEEE Transactions on Automatic Control, 1996, 41(7): 1073-1078.
  • 7Jiang B, Wang J L, Soh Y C. An adaptive technique for robust diagnosis of faults with independent effects on system outputs. International Journal of Control, 2002, 75(11): 792-802.
  • 8Wang H, Shen L. Fault detection and estimation for nonlinear systems with linear output structure. International Journal of Adaptive Control and Signal Processing, 2005, 19(4): 267-279.
  • 9Jiang B, Staroswiecki M, Cocquempot V. Fault accommodation for nonlinear dynamic systems. IEEE Transactions on Automatic Control, 2006, 51(9): 1578-1583.
  • 10Edwards C, Yan X G, Spurgeon S K. On the solvability of the constrained Lyapunov problem. IEEE Transactions on Automatic Control, 2007, 52(10): 1982-1987.

共引文献41

同被引文献30

  • 1何勇灵,陈彦民,周岷峰.四旋翼飞行器在风场扰动下的建模与控制[J].中国惯性技术学报,2013,21(5):624-630. 被引量:38
  • 2尤富强,田作华,施颂椒.Actuator fault diagnosis of time-delay systems based on adaptive observer[J].Journal of Systems Engineering and Electronics,2005,16(3):624-631. 被引量:1
  • 3Merheb A R, Noura H, Bateman F. Passive fault tolerant con- trol of quadrotor UAV using regular and cascaded sliding mode control[C] // Proc. of the IEEE Conference on Control and Fault Tolerant Systems, 2013 : 330 - 335.
  • 4Sharifi F, Mirzaei M, Gordon B W, et al. Fault tolerant control of a quadrotor UAV using sliding mode control[C]//Proc, of the IEEE Conference on Control and Fault-Tolerant Systems, 2010:239 - 244.
  • 5Madani T, Benallegue A. Backstepping control for a quadrotor helicopter[C]//Proc, of the IEEE /RSJ International Confer ence on Intelligent Robots and Systems, 2006 : 3255 - 3260.
  • 6Das A, Lewis F, Subharao K. Backstepping approach for con trolling a quadrotor using lagrange form dynamics[J]. Journal of Intelligent and Robotic Systems, 2009, 56(1/2) : 127 - 151.
  • 7Zhang X, Parisini T, Polycarpou M M. Adaptive fault tolerant control of nonlinear uncertain systems: an information-based di- agnostic approach[J]. IEEE Trans. on Automatic Control, 2004, 49(8) :1259 - 1274.
  • 8Patton R J. Fault-tolerant control systems: the 1997 situation[C]// Proc. of the IFAC Symposium on Fault Detection Supervision and Safety for Technical Processes, 1997: 1033- 1054.
  • 9Lu C H, Tsai C C. Generalized predictive control using recur- rent fuzzy neural networks for industrial processes[J]. Journal of Process Control, 2007,17 (1): 88 - 92.
  • 10Jin J, Ko S, Ryoo C K. Fault tolerant control for satellites with four reaction wheels[J]. Control Engineering Practice, 2008,16 (10) :1250 - 1258.

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