Application of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters /

Bibliographic Details
Main Author:	Kobayashi, Takahisa
Corporate Authors:	NASA Glenn Research Center, U.S. Army Research Laboratory, ASME Turbo Expo
Other Authors:	Simon, Donald L., Litt, Jonathan S.
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2005]
Series:	NASA technical memorandum ; 2005-213865.
Subjects:	Kalman filters. Aircraft engines. Gas turbine engines. Aircraft performance. Amplification.
Online Access:	https://purl.fdlp.gov/GPO/gpo20003

Description
Item Description:	Title from title screen (viewed on Mar. 12, 2012). "Prepared for the Turbo Expo 2005 sponsored by the American Society of Mechanical Engineers, Reno, Nevada, June 6-9, 2005." "September 2005." "ARL-TR-3489." "GT2005-68494." Electronic resource.
Physical Description:	1 online resource (12 pages) : color illustrations
Bibliography:	Includes bibliographical references (pages 11-12).