Active fault detection and isolation strategy for an unmanned aerial vehicle with redundant flight control surfaces

François Bateman; Hassan Noura; Mustapha Ouladsine

doi:10.1109/MED.2008.4602147

Active fault detection and isolation strategy for an unmanned aerial vehicle with redundant flight control surfaces

François Bateman, Hassan Noura, Mustapha Ouladsine

Department of Electrical and Communication Engineering

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

11 Citations (Scopus)

Abstract

In this paper, a diagnosis system using unknown input observers in order to detect, isolate and estimate faulty control surface positions for a small UAV, is presented. As this aircraft is equipped with redundant actuators, flap and aileron positions are not input observable and an active diagnosis process has to be implemented.

Original language	English
Title of host publication	2008 Mediterranean Conference on Control and Automation - Conference Proceedings, MED'08
Pages	1246-1251
Number of pages	6
DOIs	https://doi.org/10.1109/MED.2008.4602147
Publication status	Published - 2008
Event	2008 Mediterranean Conference on Control and Automation, MED'08 - Ajaccio-Corsica, France Duration: Jun 25 2008 → Jun 27 2008

Publication series

Name	2008 Mediterranean Conference on Control and Automation - Conference Proceedings, MED'08

Other

Other	2008 Mediterranean Conference on Control and Automation, MED'08
Country/Territory	France
City	Ajaccio-Corsica
Period	6/25/08 → 6/27/08

Keywords

Active diagnosis
Fault detection and isolation
Input observability
Redundant actuators
UAV
Unknown input functional decoupled observer

ASJC Scopus subject areas

Control and Systems Engineering

Access to Document

10.1109/MED.2008.4602147

Cite this

Bateman, F., Noura, H., & Ouladsine, M. (2008). Active fault detection and isolation strategy for an unmanned aerial vehicle with redundant flight control surfaces. In 2008 Mediterranean Conference on Control and Automation - Conference Proceedings, MED'08 (pp. 1246-1251). Article 4602147 (2008 Mediterranean Conference on Control and Automation - Conference Proceedings, MED'08). https://doi.org/10.1109/MED.2008.4602147

Active fault detection and isolation strategy for an unmanned aerial vehicle with redundant flight control surfaces. / Bateman, François; Noura, Hassan; Ouladsine, Mustapha.
2008 Mediterranean Conference on Control and Automation - Conference Proceedings, MED'08. 2008. p. 1246-1251 4602147 (2008 Mediterranean Conference on Control and Automation - Conference Proceedings, MED'08).

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

Bateman, F, Noura, H & Ouladsine, M 2008, Active fault detection and isolation strategy for an unmanned aerial vehicle with redundant flight control surfaces. in 2008 Mediterranean Conference on Control and Automation - Conference Proceedings, MED'08., 4602147, 2008 Mediterranean Conference on Control and Automation - Conference Proceedings, MED'08, pp. 1246-1251, 2008 Mediterranean Conference on Control and Automation, MED'08, Ajaccio-Corsica, France, 6/25/08. https://doi.org/10.1109/MED.2008.4602147

Bateman F, Noura H, Ouladsine M. Active fault detection and isolation strategy for an unmanned aerial vehicle with redundant flight control surfaces. In 2008 Mediterranean Conference on Control and Automation - Conference Proceedings, MED'08. 2008. p. 1246-1251. 4602147. (2008 Mediterranean Conference on Control and Automation - Conference Proceedings, MED'08). doi: 10.1109/MED.2008.4602147

Bateman, François ; Noura, Hassan ; Ouladsine, Mustapha. / Active fault detection and isolation strategy for an unmanned aerial vehicle with redundant flight control surfaces. 2008 Mediterranean Conference on Control and Automation - Conference Proceedings, MED'08. 2008. pp. 1246-1251 (2008 Mediterranean Conference on Control and Automation - Conference Proceedings, MED'08).

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abstract = "In this paper, a diagnosis system using unknown input observers in order to detect, isolate and estimate faulty control surface positions for a small UAV, is presented. As this aircraft is equipped with redundant actuators, flap and aileron positions are not input observable and an active diagnosis process has to be implemented.",

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Active fault detection and isolation strategy for an unmanned aerial vehicle with redundant flight control surfaces

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Keywords

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