DocumentCode
3179664
Title
Fault Detection and Isolation for Inertial Measurement Units
Author
Bras, Sergio ; Rosa, P. ; Silvestre, Carlos ; Oliveira, P.
Author_Institution
Lab. of Robot. & Syst. in Eng. & Sci. (LARSyS), Univ. Tec. de Lisboa, Lisbon, Portugal
fYear
2012
fDate
10-13 Dec. 2012
Firstpage
600
Lastpage
605
Abstract
This paper addresses the problem of Fault Detection and Isolation (FDI) for navigation systems equipped with sensors providing inertial measurements and vector observations. Two strategies are proposed. The first one takes advantage of existing hardware redundancy, providing sufficient conditions for the isolation of faults. The second approach exploits the analytical redundancy between the angular velocity measurements and the vector observations, by resorting to Set-Valued Observers (SVOs). The behavior of both strategies are illustrated in simulation.
Keywords
aircraft navigation; angular measurement; fault diagnosis; inertial navigation; observers; velocity measurement; analytical redundancy; angular velocity measurement; fault detection; fault isolation; hardware redundancy; inertial measurement unit; navigation system; set-valued observer; vector observation; Angular velocity; Noise; Noise measurement; Redundancy; Sensor systems; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control (CDC), 2012 IEEE 51st Annual Conference on
Conference_Location
Maui, HI
ISSN
0743-1546
Print_ISBN
978-1-4673-2065-8
Electronic_ISBN
0743-1546
Type
conf
DOI
10.1109/CDC.2012.6426831
Filename
6426831
Link To Document