LEADER 02184oam 2200601I 450 001 9910706187403321 005 20170818145427.0 035 $a(CKB)5470000002454550 035 $a(OCoLC)846329311 035 $a(EXLCZ)995470000002454550 100 $a20130602j199908 ua 0 101 0 $aeng 135 $aurbn||||a|a|| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aReconfigurable flight control designs with application to the X-33 vehicle /$fJohn J. Burken, Ping Lu and Zhenglu Wu 210 1$aEdwards, California :$cNational Aeronautics and Space Administration, Dryden Flight Research Center$dAugust 1999. 215 $a1 online resource (15 pages) $cillustrations 225 1 $aNASA/TM ;$v1999-206582 300 $a"August 1999." 300 $a"Presented at AIAA Guidance Navigation and Control Conference, Portland, Oregon, August 9-11, 1999, AIAA-99-4134"--Report documentation page. 300 $a"Performing organization: NASA Dryden Flight Research Center"--Report documentation page. 320 $aIncludes bibliographical references (page 15). 606 $aControl systems design$2nasat 606 $aMIMO (control systems)$2nasat 606 $aX-33 reusable launch vehicle$2nasat 606 $aServomechanisms$2nasat 606 $aProportional control$2nasat 606 $aFlight control$2nasat 606 $aLaunch vehicle configurations$2nasat 615 7$aControl systems design. 615 7$aMIMO (control systems) 615 7$aX-33 reusable launch vehicle. 615 7$aServomechanisms. 615 7$aProportional control. 615 7$aFlight control. 615 7$aLaunch vehicle configurations. 700 $aBurken$b John J.$01407949 702 $aLu$b Ping 702 $aWu$b Zhenglu 712 02$aHugh L. Dryden Flight Research Center, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCO 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910706187403321 996 $aReconfigurable flight control designs with application to the X-33 vehicle$93497634 997 $aUNINA