NASA NTRS · 19880013517
Analytical sensor redundancy assessment
Abstract
The 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.
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Mulcare, D. B., Downing, L. E., Smith, M. K.. 1988-04-01. Analytical sensor redundancy assessment. https://ntrs.nasa.gov/citations/19880013517
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