Detection of actuator faults in flight control Systems

被引：0

作者：

Chaib, S. ^{[1
]}

Saad, M. ^{[2
]}

Abou, S.C. ^{[3
]}

Boutat, D. ^{[1
]}

机构：

[1] Laboratoire Vision et Robotique, Université d'Orleans, ENSIB, Orleans, France

[2] Electrical Engineering Department, École de Technologie Superieure (ETS), Montréal, QC H3C 1K3, Canada

[3] Department of Mechanical and Industrial Engineering, University of Minnesota at Duluth, Duluth, MN 55812-3042, United States

来源：

Canadian Aeronautics and Space Journal | 2009年 / 55卷 / 03期

关键词：

A method for the multiple fault diagnosis of aircraft traditional aerodynamic control surfaces described by a nonlinear model is proposed in the form of an algorithm. A geometric approach to the nonlinear fault detection and isolation problem is investigated for actuator fault detection. The approach is based on the geometric decomposition of aircraft dynamics into tangential and transverse dynamics. Its application to reconstructed flight fault dynamics enables fault detection and distinguishes which one is occurring. To efficiently identify safety issues; critical contingencies leading the system to a failure state can be evaluated using effective algorithms within each functional area of the whole system. Results of the proposed approaches indicate not only the effective identification of faults in civil transport aircraft but also improvements in establishing an acceptable level of safety performance; even when the number of faults is not known a priori. © 2009 CASI;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Journal article (JA)

引用

页码：133 / 143

共 50 条

[21] Reliable stabilization of networked control systems with actuator faults
Hou, Yi-You
NONLINEAR DYNAMICS, 2013, 71 (03) : 447 - 455
[22] Reliable stabilization of networked control systems with actuator faults
Yi-You Hou
Nonlinear Dynamics, 2013, 71 : 447 - 455
[23] Reconfigurable Fault-Tolerant UAV Flight Control Against Actuator Faults
Hajiyev, Ch.
2016 AUSTRALIAN CONTROL CONFERENCE (AUCC), 2016, : 323 - 328
[24] Unmanned Aerial Vehicle Flight Control Evaluations Under Sensor and Actuator Faults
Chimpalthradi R. Ashokkumar
George W. P. York
Journal of Intelligent & Robotic Systems, 2017, 88 : 437 - 447
[25] Unmanned Aerial Vehicle Flight Control Evaluations Under Sensor and Actuator Faults
Ashokkumar, Chimpalthradi R.
York, George W. P.
JOURNAL OF INTELLIGENT & ROBOTIC SYSTEMS, 2017, 88 (2-4) : 437 - 447
[26] Reliable control against actuator failures of flight control systems
Yan, XJ
Gao, JY
ICEMI'2001: FIFTH INTERNATIONAL CONFERENCE ON ELECTRONIC MEASUREMENT AND INSTRUMENTS, VOL 1, CONFERENCE PROCEEDINGS, 2001, : 153 - 156
[27] Active Complementary Control for Affine Nonlinear Control Systems With Actuator Faults
Fan, Quan-Yong
Yang, Guang-Hong
IEEE TRANSACTIONS ON CYBERNETICS, 2017, 47 (11) : 3542 - 3553
[28] Fault tolerant control for quantized feedback control systems with actuator faults
Li, Zhi-Jun
Sun, De-Hui
Shi, Yun-Tao
Zhao, Ming-Yue
Nanjing Li Gong Daxue Xuebao/Journal of Nanjing University of Science and Technology, 2011, 35 (SUPPL. 2): : 67 - 71
[29] Adaptive fault-tolerant tracking control against actuator faults with application to flight control
Ye, Dan
Yang, Guang-Hong
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2006, 14 (06) : 1088 - 1096
[30] Accommodating a class of actuator failures in flight control systems
Hess, RA
Siwakosit, W
Chung, J
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2000, 23 (03) : 412 - 419

← 1 2 3 4 5 →