LEADER 02056nam  2200541I  450 
001 9910704624303321
005 20131018082628.0
035   $a(CKB)5470000002443475
035   $a(OCoLC)860980966
035   $a(EXLCZ)995470000002443475
100   $a20131018d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aReducing conservatism in aircraft engine response using conditionally active min-max limit regulators /$fRyan D. May, Sanjay Garg
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (10 pages) $cillustrations
225 1 $aNASA/TM 2012-217814
300   $aTitle from title screen (viewed Oct. 18, 2013).
300   $a"December 2012."
300   $aPrepared for the Turbo Expo 2012 sponsored by the American Society of Mechanical Engineers (ASME), Copenhagen, Denmark, June 11-15, 2012.
300   $a"GT2012-70017."
320   $aIncludes bibliographical references (page 10).
606   $aCommercial aircraft$2nasat
606   $aAircraft control$2nasat
606   $aControl systems design$2nasat
606   $aEngine control$2nasat
606   $aSequential control$2nasat
606   $aTransient response$2nasat
615  7$aCommercial aircraft.
615  7$aAircraft control.
615  7$aControl systems design.
615  7$aEngine control.
615  7$aSequential control.
615  7$aTransient response.
700   $aMay$b Ryan D.$01387409
702   $aGarg$b Sanjay
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aNASA Glenn Research Center,
712 12$aASME Turbo Expo$f(2012 :$eCopenhagen, Denmark)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704624303321
996   $aReducing conservatism in aircraft engine response using conditionally active min-max limit regulators$93507608
997   $aUNINA