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100   $a20110613d2010      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLoop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds$b[electronic resource] /$fJoseph W. Connolly and George Kopasakis ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010]
215   $a1 online resource (19 pages) $cillustrations (color)
225 1 $aNASA/TM ;$v2010-216897
300   $aTitle from title screen (viewed on June 13, 2011).
300   $a"October 2010."
300   $a"AIAA-2010-7068."
320   $aIncludes bibliographical references (pages 18-19).
517   $aLoop Shaping control design for a supersonic propulsion system model using quantitative feedback theory 
606   $aSupersonic flight$2nasat
606   $aControl systems design$2nasat
606   $aSupersonic transports$2nasat
606   $aSpecifications$2nasat
606   $aSupersonic inlets$2nasat
606   $aDynamic models$2nasat
606   $aLoops$2nasat
606   $aFeedback control$2nasat
606   $aSupersonic wind tunnels$2nasat
606   $aFlow distribution$2nasat
606   $aComputational fluid dynamics$2nasat
615  7$aSupersonic flight.
615  7$aControl systems design.
615  7$aSupersonic transports.
615  7$aSpecifications.
615  7$aSupersonic inlets.
615  7$aDynamic models.
615  7$aLoops.
615  7$aFeedback control.
615  7$aSupersonic wind tunnels.
615  7$aFlow distribution.
615  7$aComputational fluid dynamics.
700   $aConnolly$b Joseph W$01398989
701   $aKopasakis$b George$01395866
712 02$aNASA Glenn Research Center.
712 12$aAIAA/ASME/SAE/ASEE Joint Propulsion Conference$d(46th :$f2010 :$eNashville, Tenn.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700358203321
996   $aLoop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds$93463398
997   $aUNINA