02045oam 2200517 450 991070795420332120170202134330.0(CKB)5470000002469026(OCoLC)703663040(EXLCZ)99547000000246902620110224j199211 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierSubsonic flight test evaluation of a propulsion system parameter estimation process for the F-100 engine /John S. Orme and Glenn B. Gilyard[Washington, D.C.] :National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,November 1992.1 online resource (24 pages) illustrationsNASA technical memorandum ;4426"November 1992" Report Documentation page."Performing organization: NASA Dryden Flight Research Facility"-- Report Documentation page.Includes bibliographical references (pages 12-13).Adaptive controlnasatAircraft performancenasatF-15 aircraftnasatKalman filtersnasatOptimal controlnasatPropulsion system performancenasatAdaptive control.Aircraft performance.F-15 aircraft.Kalman filters.Optimal control.Propulsion system performance.Orme John S.1387567Gilyard Glenn B.Dryden Flight Research Facility.United States.National Aeronautics and Space Administration.Scientific and Technical Information Program,SSNSSNGPOBOOK9910707954203321Subsonic flight test evaluation of a propulsion system parameter estimation process for the F-100 engine3437554UNINA