NASA NTRS · 19820005272
Sensor failure detection system
Abstract
Advanced concepts for detecting, isolating, and accommodating sensor failures were studied to determine their applicability to the gas turbine control problem. Five concepts were formulated based upon such techniques as Kalman filters and a screening process led to the selection of one advanced concept for further evaluation. The selected advanced concept uses a Kalman filter to generate residuals, a weighted sum square residuals technique to detect soft failures, likelihood ratio testing of a bank of Kalman filters for isolation, and reconfiguring of the normal mode Kalman filter by eliminating the failed input to accommodate the failure. The advanced concept was compared to a baseline parameter synthesis technique. The advanced concept was shown to be a viable concept for detecting, isolating, and accommodating sensor failures for the gas turbine applications.
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Beattie, E. C., Laprad, R. F., Mcglone, M. E., Rock, S. M., Akhter, M. M.. 1981-08-01. Sensor failure detection system. https://ntrs.nasa.gov/citations/19820005272
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