02056nam 2200541I 450 991070462430332120131018082628.0(CKB)5470000002443475(OCoLC)860980966(EXLCZ)99547000000244347520131018d2012 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierReducing conservatism in aircraft engine response using conditionally active min-max limit regulators /Ryan D. May, Sanjay GargCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2012]1 online resource (10 pages) illustrationsNASA/TM 2012-217814Title from title screen (viewed Oct. 18, 2013)."December 2012."Prepared for the Turbo Expo 2012 sponsored by the American Society of Mechanical Engineers (ASME), Copenhagen, Denmark, June 11-15, 2012."GT2012-70017."Includes bibliographical references (page 10).Commercial aircraftnasatAircraft controlnasatControl systems designnasatEngine controlnasatSequential controlnasatTransient responsenasatCommercial aircraft.Aircraft control.Control systems design.Engine control.Sequential control.Transient response.May Ryan D.1387409Garg SanjayUnited States.National Aeronautics and Space Administration,NASA Glenn Research Center,ASME Turbo Expo(2012 :Copenhagen, Denmark)GPOGPOBOOK9910704624303321Reducing conservatism in aircraft engine response using conditionally active min-max limit regulators3507608UNINA