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Analytical sensor redundancy assessmentThe rationale and mechanization of sensor fault tolerance based on analytical redundancy principles are described. The concept involves the substitution of software procedures, such as an observer algorithm, to supplant additional hardware components. The observer synthesizes values of sensor states in lieu of their direct measurement. Such information can then be used, for example, to determine which of two disagreeing sensors is more correct, thus enhancing sensor fault survivability. Here a stability augmentation system is used as an example application, with required modifications being made to a quadruplex digital flight control system. The impact on software structure and the resultant revalidation effort are illustrated as well. Also, the use of an observer algorithm for wind gust filtering of the angle-of-attack sensor signal is presented.
Document ID
19880013517
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mulcare, D. B.
(Lockheed-Georgia Co. Marietta, GA, United States)
Downing, L. E.
(Lockheed-Georgia Co. Marietta, GA, United States)
Smith, M. K.
(Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1988
Subject Category
Aircraft Instrumentation
Report/Patent Number
NAS 1.26:182892
NASA-CR-182892
DOT/FAA/CT-86/32
Report Number: NAS 1.26:182892
Report Number: NASA-CR-182892
Report Number: DOT/FAA/CT-86/32
Accession Number
88N22901
Funding Number(s)
CONTRACT_GRANT: NAS2-11853
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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