JOURNAL OF SHANDONG UNIVERSITY (ENGINEERING SCIENCE) ›› 2017, Vol. 47 ›› Issue (5): 166-172.doi: 10.6040/j.issn.1672-3961.0.2017.195
Previous Articles Next Articles
DENG Junwu, ZHANG Yumin*, ZHANG Hongdi, DU Xiaokun
CLC Number:
[1] 陈宗基, 张汝麟, 张平,等. 飞行器控制面临的机遇与挑战[J]. 自动化学报, 2013, 39(6):703-710. CHEN Zongji, ZHANG Rulin, ZHANG Ping, et al. Flight control: challenges and opportunities[J]. Acta Automatica Sinica, 2013, 39(6):703-710. [2] ISERMANN R. Fault-diagnosis systems: an introduction from fault detection to fault tolerance[M]. Berlin: Springer, 2006. [3] DE LOZA A F, CIESLAK J, HENRY D, et al. Sensor fault diagnosis using a non-homogeneous high-order sliding mode observer with application to a transport aircraft[J]. Iet Control Theory & Applications, 2015, 9(4):598-607. [4] 胡志坤, 孙岩, 姜斌,等. 一种基于最优未知输入观测器的故障诊断方法[J]. 自动化学报, 2013, 39(8):1225-1230. HU Zhikun, SUN Yan, JIANG Bin, et al. An optimal unknown input observer based fault diagnosis method[J]. Acta Automatica Sinica, 2013, 39(8):1225-1230. [5] CHADLI M, ABDO A, DING S X. H-/H∞fault detection filter design for discrete-time Takagi-Sugeno fuzzy system[J]. Automatica, 2013, 49(7): 1996-2005. [6] 叶慧, 罗秋凤, 李勇. 小波和多核SVM方法在UVA传感器故障诊断的应用[J]. 电子测量技术, 2014, 37(1):112-116. YE Hui, LUO Qiufeng, LI Yong. Application of wavelet and multi-kernel SVM in UAV sensors fault diagnosis[J]. Electronic Measurement Technology, 2014, 37(1):112-116. [7] NAPOLITANO M R, CHEN C I, NAYLOR S. Aircraft failure detection and identification using neural networks[J]. Journal of Guidance, Control, and Dynamics, 2015, 16(6):999-1009. [8] KAMALI C, PASHILKAR A A, RAOI J R. Evaluation of recursive least squares algorithm for parameter estimation in aircraft real time applications[J]. Aerospace Science and Technology, 2011, 15(3):165-174. [9] LOMBAERTS T, OORT E V, CHU Q P, et al. Online aerodynamic model structure selection and parameter estimation for fault tolerant control[J]. Journal of Guidance, Control, and Dynamics, 2012, 33(3):707-723. [10] 陈敏泽, 周东华. 一种基于强跟踪滤波器的自适应故障预报方法[J]. 上海海事大学学报, 2001, 22(3):35-40. CHEN Minze, ZHOU Donghua. Adaptive fault prediction method based on strong tracking filter[J]. Journal of Shanghai Maritime University, 2001, 22(3):35-40. [11] CARMINATI M, FERRARI G, GRASSETTI R, et al. Real-time data fusion and MEMS sensors fault detection in an aircraft emergency attitude unit based on Kalman filtering[J]. IEEE Sensors Journal, 2011, 12(10):2984-2992. [12] 耿淼, 姜斌, 郭玉英,等. 执行器故障参数不可测飞行系统的模型跟踪重构控制[J]. 东南大学学报(自然科学版), 2009(S1):177-182. GENG Miao, JIANG Bin, GUO Yuying, et al. Model following reconfigurable flight control in the presence of actuator faults with non-measurable rates[J]. Journal of Southeast University(Natural Science Edition), 2009(S1):177-182. [13] SHI Z B, SUN D, LIU T, et al. Fault-tolerant reconfiguration of flight control system based on pseudo-inverse and optimal method[J]. Journal of Civil Aviation University of China, 2014. [14] 周东华. 现代故障诊断与容错控制[M]. 北京:清华大学出版社, 2000. |
[1] | LI Hongyang, HE Xiao. A fault detection and estimation scheme for nonlinear stochastic systems based on SCKF [J]. JOURNAL OF SHANDONG UNIVERSITY (ENGINEERING SCIENCE), 2017, 47(5): 130-135. |
|