DocumentCode
184091
Title
A sensor fault detection for aircraft using a single Kalman filter and hidden Markov models
Author
Rudin, Konrad ; Ducard, Guillaume J. J. ; Siegwart, Roland Y.
Author_Institution
Autonomous Syst. Lab. (ASL), Zürich, Switzerland
fYear
2014
fDate
8-10 Oct. 2014
Firstpage
991
Lastpage
996
Abstract
This paper presents a new scheme for sensor fault detection and isolation. It uses a single Kalman filter and a Gaussian hidden Markov model for each of the monitored sensors. This combination is able to simultaneously detect single and multiple sensor faults, still guaranteeing optimal system state estimation. This algorithm also can run on systems with limited computational power. The efficiency of the approach is evaluated through simulation of an aircraft to detect airspeed and GPS sensor faults. The results show fast fault detection and low false-alarm rate.
Keywords
Gaussian processes; Global Positioning System; Kalman filters; aircraft; autonomous aerial vehicles; fault diagnosis; hidden Markov models; sensors; state estimation; GPS sensor faults; Gaussian hidden Markov model; airspeed sensor faults; computational power; false-alarm rate; optimal system state estimation; sensor fault detection; sensor fault isolation; single Kalman filter; Covariance matrices; Fault detection; Global Positioning System; Hidden Markov models; Quaternions; Technological innovation; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications (CCA), 2014 IEEE Conference on
Conference_Location
Juan Les Antibes
Type
conf
DOI
10.1109/CCA.2014.6981464
Filename
6981464
Link To Document