Özet
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.
| Orijinal dil | İngilizce |
|---|---|
| Sayfa (başlangıç-bitiş) | 127-139 |
| Sayfa sayısı | 13 |
| Dergi | Kybernetes |
| Hacim | 39 |
| Basın numarası | 1 |
| DOI'lar | |
| Yayın durumu | Yayınlandı - 2010 |
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