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Virtual sensor for fault detection and isolation in flight control systems - fuzzy modeling approach

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2 Author(s)
Oosterom, M. ; Control Eng. Lab., Delft Univ. of Technol., Netherlands ; Babuska, R.

A virtual sensor for normal acceleration has been developed and implemented in the flight control system of a small commercial aircraft. The inputs of the virtual sensor are the consolidated outputs of dissimilar sensor signals. The virtual sensor is a fuzzy model of the Takagi-Sugeno type and it has been identified from simulated data, using a detailed, realistic Matlab/SimulinkTM model used by the aircraft manufacturer. This virtual sensor can be applied to identify a failed sensor in the case that only two real sensors are available and even to detect a failure of the last available sensor

Published in:
Decision and Control, 2000. Proceedings of the 39th IEEE Conference on  (Volume:3 )

Date of Conference: 2000

Page(s):
2645 - 2650 vol.3
Meeting Date :
12 Dec 2000-15 Dec 2000
ISSN :
0191-2216
Print ISBN:
0-7803-6638-7
INSPEC Accession Number:
6964881
Conference Location :
Sydney, NSW
Digital Object Identifier :
10.1109/CDC.2000.914204
Product Type:
Conference Publications

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