LEADER 01805nam  2200433Ia 450 
001 9910697023503321
005 20230902161938.0
035   $a(CKB)5470000002384670
035   $a(OCoLC)654839461
035   $a(EXLCZ)995470000002384670
100   $a20100811d2005      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn optimal orthogonal decomposition method for Kalman filter-based turbofan engine thrust estimation$b[electronic resource] /$fJonathan S. Litt ; prepared for the Turbo Expo 2005 sponsored by the American Society of Mechanical Engineers, Reno, Nevada, June 6-9, 2005
210  1$aCleveland, Ohio :$cU.S. Army Research Laboratory, National Aeronautics and Space Administration, Glenn Research Center,$d[2005]
215   $a1 online resource (11 pages, 1 unnumbered page) $cillustrations
225 1 $aNASA/TM ;$v2005-213864
300   $aTitle from PDF title screen (NASA, viewed July 21, 2010).
300   $a"October 2005."
300   $a"ARL-TR-3487."
300   $a"GT2005-68808."
320   $aIncludes bibliographical references.
410  0$aNASA technical memorandum ;$v2005-213864.
606   $aAirplanes$xMotors$xThrust$xMeasurement$vCongresses
608   $aConference papers and proceedings.$2lcgft
615  0$aAirplanes$xMotors$xThrust$xMeasurement
700   $aLitt$b Jonathan S$01398039
712 02$aU.S. Army Research Laboratory.
712 02$aNASA Glenn Research Center.
712 12$aASME Turbo Expo.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697023503321
996   $aAn optimal orthogonal decomposition method for Kalman filter-based turbofan engine thrust estimation$93535739
997   $aUNINA