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Failure detection and fault management techniques for flush airdata sensing systemsMethods based on chi-squared analysis are presented for detecting system and individual-port failures in the high-angle-of-attack flush airdata sensing system on the NASA F-18 High Alpha Research Vehicle. The HI-FADS hardware is introduced, and the aerodynamic model describes measured pressure in terms of dynamic pressure, angle of attack, angle of sideslip, and static pressure. Chi-squared analysis is described in the presentation of the concept for failure detection and fault management which includes nominal, iteration, and fault-management modes. A matrix of pressure orifices arranged in concentric circles on the nose of the aircraft indicate the parameters which are applied to the regression algorithms. The sensing techniques are applied to the F-18 flight data, and two examples are given of the computed angle-of-attack time histories. The failure-detection and fault-management techniques permit the matrix to be multiply redundant, and the chi-squared analysis is shown to be useful in the detection of failures.
Document ID
19920043095
Document Type
Conference Paper
Authors
Whitmore, Stephen A. (NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Moes, Timothy R. (NASA Flight Research Center Edwards, CA, United States)
Leondes, Cornelius T. (Washington, University Seattle, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
AIRCRAFT INSTRUMENTATION
Report/Patent Number
AIAA PAPER 92-0263
Distribution Limits
Public
Copyright
Other