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2015 | 25 | 1 | 189-201
Tytuł artykułu

SMAC-FDI: A single model active fault detection and isolation system for unmanned aircraft

Treść / Zawartość
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
This article presents a single model active fault detection and isolation system (SMAC-FDI) which is designed to efficiently detect and isolate a faulty actuator in a system, such as a small (unmanned) aircraft. This FDI system is based on a single and simple aerodynamic model of an aircraft in order to generate some residuals, as soon as an actuator fault occurs. These residuals are used to trigger an active strategy based on artificial exciting signals that searches within the residuals for the signature of an actuator fault. Fault isolation is carried out through an innovative mechanism that does not use the previous residuals but the actuator control signals directly. In addition, the paper presents a complete parameter-tuning strategy for this FDI system. The novel concepts are backed-up by simulations of a small unmanned aircraft experiencing successive actuator failures. The robustness of the SMAC-FDI method is tested in the presence of model uncertainties, realistic sensor noise and wind gusts. Finally, the paper concludes with a discussion on the computational efficiency of the method and its ability to run on small microcontrollers.
Rocznik
Tom
25
Numer
1
Strony
189-201
Opis fizyczny
Daty
wydano
2015
otrzymano
2014-02-20
poprawiono
2014-09-08
Twórcy
  • CNRS, I3S, UMR 7271, University of Nice Sophia Antipolis, 2000 Route des Lucioles, Bat. Euclide B, Les Algorithmes, 06903 Sophia Antipolis, France
Bibliografia
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Typ dokumentu
Bibliografia
Identyfikatory
Identyfikator YADDA
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