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Filter failure detection for systems with large space structure dynamicsA failure detection filter is applied to the detection of actuator and sensor failures on a free-free beam. Computer simulation tests are used to verify the filter design and study the effect of unmodeled modes on filter performance. In actuator tests, the failure signal to spillover noise ratio was found to be greatest when the filter bandwidth was 5 rad/sec beyond the input frequency. Observation spillover, however, was found to vary widely in tests run under similar conditions (same input frequency and filter poles) but with different detector gains. In sensor tests, the maximum signal-to-noise ratio for varying filter bandwidth depended upon the initial conditions placed on the unmodeled modes; the performance was good even for initial amplitudes on the first unmodeled mode 7.5% of that on the last modeled mode.
Document ID
19820021468
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Carignan, C. R.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1982
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
SSL-1-82
NASA-CR-169146
NAS 1.26:169146
Report Number: SSL-1-82
Report Number: NASA-CR-169146
Report Number: NAS 1.26:169146
Accession Number
82N29344
Funding Number(s)
CONTRACT_GRANT: NAG1-126
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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