Application of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters / Takahisa Kobayashi, Donald L. Simon and Jonathan S. Litt.

Author/creator Kobayashi, Takahisa
Format Electronic
Publication InfoCleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2005]
Description1 online resource (12 p.) : col. ill.
Supplemental Contenthttps://purl.fdlp.gov/GPO/gpo20003

Other author/creatorSimon, Donald L.
Other author/creatorLitt, Jonathan S.
Other author/creatorNASA Glenn Research Center.
Other author/creatorU.S. Army Research Laboratory.
Other author/creatorASME Turbo Expo (2005 : Reno, Nev.)
SeriesNASA/TM ; 2005-213865
NASA technical memorandum 2005-213865. ^A467613
General noteTitle from title screen (viewed on Mar. 12, 2012).
General note"Prepared for the Turbo Expo 2005 sponsored by the American Society of Mechanical Engineers, Reno, Nevada, June 6-9, 2005."
General note"September 2005."
General note"ARL-TR-3489."
General note"GT2005-68494."
General noteGPO Cataloging Record Distribution Program (CRDP).
Bibliography noteIncludes bibliographical references (p. 11-12).
Funding informationSponsored by National Aeronautics and Space Administration and U.S. Army Research Laboratory WBS-22-079-30-05 1L161102AF20 E-15235
GPO item number0830-D (online)
Govt. docs number NAS 1.15:2005-213865

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Electronic Resources Access Content Online ✔ Available