02111nam 2200541Ia 450 991070147350332120120312094145.0(CKB)5470000002418340(OCoLC)779847140(EXLCZ)99547000000241834020120312d2005 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierApplication of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters[electronic resource] / Takahisa Kobayashi, Donald L. Simon and Jonathan S. LittCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2005]1 online resource (12 pages) color illustrationsNASA/TM ;2005-213865Title 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."Includes bibliographical references (pages 11-12).Kalman filtersnasatAircraft enginesnasatGas turbine enginesnasatAircraft performancenasatAmplificationnasatKalman filters.Aircraft engines.Gas turbine engines.Aircraft performance.Amplification.Kobayashi Takahisa1419547Simon Donald L1389758Litt Jonathan S1398039NASA Glenn Research Center.U.S. Army Research Laboratory.ASME Turbo Expo(2005 :Reno, Nev.)GPOGPOBOOK9910701473503321Application of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters3534398UNINA