LEADER 01823oam  2200529I  450 
001 9910704484703321
005 20130226161029.0
035   $a(CKB)5470000002440845
035   $a(OCoLC)828565798
035   $a(EXLCZ)995470000002440845
100   $a20130226d1986      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDesign and verification by nonlinear simulation of a Mach/CAS control law for the NASA TSRV B-737 aircraft $efinal report /$fKevin R. Bruce
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[1986]
215   $a1 online resource (i, 65 pages) $cillustrations
225 1 $aNASA CR ;$v178029
300   $aTitle from title screen (viewed on Feb. 26, 2013).
300   $a"August 1986."
320   $aIncludes bibliographical references (page 20).
517   $aDesign and verification by nonlinear simulation of a Mach/CAS control law for the NASA TSRV B-737 aircraft 
606   $aAirspeed$2nasat
606   $aCalibrating$2nasat
606   $aFlight control$2nasat
606   $aFlight management systems$2nasat
606   $aNonlinear systems$2nasat
606   $aProfiles$2nasat
606   $aSimulation$2nasat
615  7$aAirspeed.
615  7$aCalibrating.
615  7$aFlight control.
615  7$aFlight management systems.
615  7$aNonlinear systems.
615  7$aProfiles.
615  7$aSimulation.
700   $aBruce$b Kevin R.$01403090
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910704484703321
996   $aDesign and verification by nonlinear simulation of a Mach$93474915
997   $aUNINA