Actuators fault diagnosis and tolerant control for an unmanned aerial vehicle

François Bateman; Hassan Noura; Mustapha Ouladsine

doi:10.1109/CCA.2007.4389374

Actuators fault diagnosis and tolerant control for an unmanned aerial vehicle

François Bateman, Hassan Noura, Mustapha Ouladsine

Department of Electrical and Communication Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

27 Citations (Scopus)

Abstract

In this paper a fault detection and isolation (FDI) method coupled with a fault tolerant control system are developed in order to deal with control surface failures for an Unmanned Aerial Vehicle (UAV). The failures considered are stuck control surfaces which occur during the aircraft manoeuvres: turn, velocity and slope variations. These faults are difficult to detect and to isolate. On the one hand they are soft variations and the aircraft is equipped with a controller which mask them, on the other hand redundancies offered by the control surfaces cause problems of isolability. The Fault Detection and Isolation system proposed here is based on a signal processing approach and drives a Fault Tolerant Control System (FTCS) built with a bank of Linear Quadratic controllers.

Original language	English
Title of host publication	16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control
Pages	1061-1066
Number of pages	6
DOIs	https://doi.org/10.1109/CCA.2007.4389374
Publication status	Published - 2007
Event	16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control - , Singapore Duration: Oct 1 2007 → Oct 3 2007

Publication series

Name	Proceedings of the IEEE International Conference on Control Applications

Other

Other	16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control
Country/Territory	Singapore
Period	10/1/07 → 10/3/07

ASJC Scopus subject areas

Engineering(all)

Access to Document

10.1109/CCA.2007.4389374

Cite this

Bateman, F., Noura, H., & Ouladsine, M. (2007). Actuators fault diagnosis and tolerant control for an unmanned aerial vehicle. In 16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control (pp. 1061-1066). [4389374] (Proceedings of the IEEE International Conference on Control Applications). https://doi.org/10.1109/CCA.2007.4389374

Actuators fault diagnosis and tolerant control for an unmanned aerial vehicle. / Bateman, François; Noura, Hassan; Ouladsine, Mustapha.
16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control. 2007. p. 1061-1066 4389374 (Proceedings of the IEEE International Conference on Control Applications).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Bateman, F, Noura, H & Ouladsine, M 2007, Actuators fault diagnosis and tolerant control for an unmanned aerial vehicle. in 16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control., 4389374, Proceedings of the IEEE International Conference on Control Applications, pp. 1061-1066, 16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control, Singapore, 10/1/07. https://doi.org/10.1109/CCA.2007.4389374

Bateman F, Noura H, Ouladsine M. Actuators fault diagnosis and tolerant control for an unmanned aerial vehicle. In 16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control. 2007. p. 1061-1066. 4389374. (Proceedings of the IEEE International Conference on Control Applications). doi: 10.1109/CCA.2007.4389374

@inproceedings{cea031384cec4592968ace082b014c00,

title = "Actuators fault diagnosis and tolerant control for an unmanned aerial vehicle",

abstract = "In this paper a fault detection and isolation (FDI) method coupled with a fault tolerant control system are developed in order to deal with control surface failures for an Unmanned Aerial Vehicle (UAV). The failures considered are stuck control surfaces which occur during the aircraft manoeuvres: turn, velocity and slope variations. These faults are difficult to detect and to isolate. On the one hand they are soft variations and the aircraft is equipped with a controller which mask them, on the other hand redundancies offered by the control surfaces cause problems of isolability. The Fault Detection and Isolation system proposed here is based on a signal processing approach and drives a Fault Tolerant Control System (FTCS) built with a bank of Linear Quadratic controllers.",

author = "Fran{\c c}ois Bateman and Hassan Noura and Mustapha Ouladsine",

year = "2007",

doi = "10.1109/CCA.2007.4389374",

language = "English",

isbn = "1424404436",

series = "Proceedings of the IEEE International Conference on Control Applications",

pages = "1061--1066",

booktitle = "16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control",

note = "16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control ; Conference date: 01-10-2007 Through 03-10-2007",

}

TY - GEN

T1 - Actuators fault diagnosis and tolerant control for an unmanned aerial vehicle

AU - Bateman, François

AU - Noura, Hassan

AU - Ouladsine, Mustapha

PY - 2007

Y1 - 2007

N2 - In this paper a fault detection and isolation (FDI) method coupled with a fault tolerant control system are developed in order to deal with control surface failures for an Unmanned Aerial Vehicle (UAV). The failures considered are stuck control surfaces which occur during the aircraft manoeuvres: turn, velocity and slope variations. These faults are difficult to detect and to isolate. On the one hand they are soft variations and the aircraft is equipped with a controller which mask them, on the other hand redundancies offered by the control surfaces cause problems of isolability. The Fault Detection and Isolation system proposed here is based on a signal processing approach and drives a Fault Tolerant Control System (FTCS) built with a bank of Linear Quadratic controllers.

AB - In this paper a fault detection and isolation (FDI) method coupled with a fault tolerant control system are developed in order to deal with control surface failures for an Unmanned Aerial Vehicle (UAV). The failures considered are stuck control surfaces which occur during the aircraft manoeuvres: turn, velocity and slope variations. These faults are difficult to detect and to isolate. On the one hand they are soft variations and the aircraft is equipped with a controller which mask them, on the other hand redundancies offered by the control surfaces cause problems of isolability. The Fault Detection and Isolation system proposed here is based on a signal processing approach and drives a Fault Tolerant Control System (FTCS) built with a bank of Linear Quadratic controllers.

UR - http://www.scopus.com/inward/record.url?scp=43049176685&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=43049176685&partnerID=8YFLogxK

U2 - 10.1109/CCA.2007.4389374

DO - 10.1109/CCA.2007.4389374

M3 - Conference contribution

AN - SCOPUS:43049176685

SN - 1424404436

SN - 9781424404438

T3 - Proceedings of the IEEE International Conference on Control Applications

SP - 1061

EP - 1066

BT - 16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control

T2 - 16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control

Y2 - 1 October 2007 through 3 October 2007

ER -

Actuators fault diagnosis and tolerant control for an unmanned aerial vehicle

Abstract

Publication series

Other

ASJC Scopus subject areas

Access to Document

Other files and links

Fingerprint

Cite this