An optimal orthogonal decomposition method for Kalman filter-based turbofan engine thrust estimation

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Main Author: Litt, Jonathan S.
Corporate Authors: U.S. Army Research Laboratory.
NASA Glenn Research Center.

ASME Turbo Expo.
Format: Book Electronic
Published:Cleveland, Ohio : U.S. Army Research Laboratory, National Aeronautics and Space Administration, Glenn Research Center, [2005]
Series:NASA technical memorandum ; 2005-213864.
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University of Illinois at Urbana-Champaign

Location: *Government Documents Online Collection

Call Number: ONLINEDOC. NAS 1.15:2005-213864