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Fault Detection Using Propagator for Kalman Filter and Its Application to SDINS

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dc.contributor.authorYu, Jaejong-
dc.contributor.authorLee, Jang Gyu-
dc.contributor.authorPark, Chan Gook-
dc.date.accessioned2009-10-06-
dc.date.available2009-10-06-
dc.date.issued2003-
dc.identifier.citationICCAS, 2003.en
dc.identifier.urihttps://hdl.handle.net/10371/10178-
dc.description.abstractIn this paper, we propose a fault detection method for extended Kalman filter in decentralized filter structure. To detect a
fault, a consistency between filter output and a monitoring signal is tested. State propagators are used to obtain the monitoring
signal. However, the output of state propagator increases in magnitude and finally diverges as time runs. To solve such problem,
two-propagator method was proposed for linear system. Two propagators are reset by Kalman filter output, alternatively, to avoid
divergence. But a test statistics change abruptly at the reset instant in that method. Hence a N-step propagator method is proposed
to fix up the problem. In the N-step propagator, only time propagations are performed from k-N+1 step to k step without
measurement updates. A test statistics are defined by errors and its covariance between extended Kalman filter and N-step
propagator. These fault detection methods are applied to integrated strapdown inertial navigation system (SDINS). By computer
simulation, it is shown that the proposed methods detect a fault effectively.
en
dc.description.sponsorshipACRC/ADDen
dc.language.isoen-
dc.subjectdecentralized filteren
dc.subjectextended Kalman filteren
dc.subjectfault detectionen
dc.subjectintegrated navigation systemen
dc.subjectSDINSen
dc.titleFault Detection Using Propagator for Kalman Filter and Its Application to SDINSen
dc.typeConference Paperen
dc.contributor.AlternativeAuthor유재종-
dc.contributor.AlternativeAuthor이장규-
dc.contributor.AlternativeAuthor박찬국-
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College of Engineering/Engineering Practice School (공과대학/대학원)Dept. of Mechanical Aerospace Engineering (기계항공공학부)Others_기계항공공학부
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