Özet
In this paper, for multidimensional dynamic systems a sensor fault detection algorithm based on the confidence interval of the generalized variance of the Kalman filter innovation sequence, is presented. The longitudinal dynamics of an aircraft control system, as an example, is considered, and detection of the fault in the air velocity sensor affecting the covariance matrix of the Kalman filter is examined.
Orijinal dil | İngilizce |
---|---|
Sayfa (başlangıç-bitiş) | 109-113 |
Sayfa sayısı | 5 |
Dergi | Proceedings of the American Control Conference |
Hacim | 1 |
Yayın durumu | Yayınlandı - 1999 |
Etkinlik | Proceedings of the 1999 American Control Conference (99ACC) - San Diego, CA, USA Süre: 2 Haz 1999 → 4 Haz 1999 |