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NASA NTRS · 19930000234

Kalman-Filter Estimation Of Unmeasured Output Variables

Abstract

Kalman-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.

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BibTeXRIS

Gilyard, Glenn B., Alag, Gurbux S.. 1993-04-01. Kalman-Filter Estimation Of Unmeasured Output Variables. https://ntrs.nasa.gov/citations/19930000234

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