LEADER 02111nam  2200541Ia 450 
001 9910701473503321
005 20120312094145.0
035   $a(CKB)5470000002418340
035   $a(OCoLC)779847140
035   $a(EXLCZ)995470000002418340
100   $a20120312d2005      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aApplication of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters$b[electronic resource] / Takahisa Kobayashi, Donald L. Simon and Jonathan S. Litt
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2005]
215   $a1 online resource (12 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2005-213865
300   $aTitle from title screen (viewed on Mar. 12, 2012).
300   $a"Prepared for the Turbo Expo 2005 sponsored by the American Society of Mechanical Engineers, Reno, Nevada, June 6-9, 2005."
300   $a"September 2005."
300   $a"ARL-TR-3489."
300   $a"GT2005-68494."
320   $aIncludes bibliographical references (pages 11-12).
606   $aKalman filters$2nasat
606   $aAircraft engines$2nasat
606   $aGas turbine engines$2nasat
606   $aAircraft performance$2nasat
606   $aAmplification$2nasat
615  7$aKalman filters.
615  7$aAircraft engines.
615  7$aGas turbine engines.
615  7$aAircraft performance.
615  7$aAmplification.
700   $aKobayashi$b Takahisa$01419547
701   $aSimon$b Donald L$01389758
701   $aLitt$b Jonathan S$01398039
712 02$aNASA Glenn Research Center.
712 02$aU.S. Army Research Laboratory.
712 12$aASME Turbo Expo$f(2005 :$eReno, Nev.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701473503321
996   $aApplication of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters$93534398
997   $aUNINA