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Kalman-Filter Estimation Of Unmeasured Output VariablesKalman-filter "observer" algorithm used in estimating unmeasured output variables of turbofan engine. Unmeasured output variables needed along with measured output variables as feedback data to characterize state of aircraft-and-engine system for control purposes. Subsystem or processor implementing Kalman-filter algorithm incorporated into adaptive digital control system, called "performance-seeking" control system, developed to compute engine-control settings to optimize performance of aircraft under given pseudo-steady-state cruise conditions. Basic concept of algorithm not restricted to aircraft-engine application and can be extended to internal-combustion engines in land vehicles.
Document ID
19930000234
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Gilyard, Glenn B.
(Dryden Flight Research Facility)
Alag, Gurbux S.
(PRC Systems Services Co.)
Date Acquired
August 16, 2013
Publication Date
April 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 4
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
ARC-12913
Report Number: ARC-12913
ISSN: 0145-319X
Accession Number
93B10234
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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