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100   $a20110224j199211    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSubsonic flight test evaluation of a propulsion system parameter estimation process for the F-100 engine /$fJohn S. Orme and Glenn B. Gilyard
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dNovember 1992.
215   $a1 online resource (24 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4426
300   $a"November 1992" Report Documentation page.
300   $a"Performing organization: NASA Dryden Flight Research Facility"-- Report Documentation page.
320   $aIncludes bibliographical references (pages 12-13).
606   $aAdaptive control$2nasat
606   $aAircraft performance$2nasat
606   $aF-15 aircraft$2nasat
606   $aKalman filters$2nasat
606   $aOptimal control$2nasat
606   $aPropulsion system performance$2nasat
615  7$aAdaptive control.
615  7$aAircraft performance.
615  7$aF-15 aircraft.
615  7$aKalman filters.
615  7$aOptimal control.
615  7$aPropulsion system performance.
700   $aOrme$b John S.$01387567
702   $aGilyard$b Glenn B.
712 02$aDryden Flight Research Facility.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
801  0$bSSN
801  1$bSSN
801  2$bGPO
906   $aBOOK
912   $a9910707954203321
996   $aSubsonic flight test evaluation of a propulsion system parameter estimation process for the F-100 engine$93437554
997   $aUNINA