Abstract
Purpose: The purpose of this paper is to design the fault detection algorithm for multidimensional dynamic systems using a new approach for checking the statistical characteristics of Kalman filter innovation sequence. Design/methodology/approach: The proposed approach is based on given statistics for the mathematical expectation of the spectral norm of the normalized innovation matrix of the Kalman filter. Findings: The longitudinal dynamics of an aircraft as an example is considered, and detection of various sensor faults affecting the mean and variance of the innovation sequence is examined. Research limitations/implications: A real-time detection of sensor faults affecting the mean and variance of the innovation sequence, applied to the linearized aircraft longitudinal dynamics, is examined. The non-linear longitudinal dynamics model of an aircraft is linearized. Faults affecting the covariances of the innovation sequence are not considered in the paper. Originality/value: The proposed approach permits simultaneous real-time checking of the expected value and the variance of the innovation sequence and does not need a priori information about statistical characteristics of this sequence in the failure case.
Original language | English |
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Pages (from-to) | 127-139 |
Number of pages | 13 |
Journal | Kybernetes |
Volume | 39 |
Issue number | 1 |
DOIs | |
Publication status | Published - 2010 |
Keywords
- Aerodynamics
- Cybernetics
- Failure modes and effects analysis
- Sensors