LEADER 01842oam 2200529I 450 001 9910706591203321 005 20171114104122.0 035 $a(CKB)5470000002456531 035 $a(OCoLC)858273830 035 $a(EXLCZ)995470000002456531 100 $a20130912j200108 ca 0 101 0 $aeng 135 $aurbn||||a|a|| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aReconfigurable control design for the full X-33 flight envelope /$fM. Christopher Cotting and John J. Burken 210 1$aEdwards, California :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$dAugust 2001. 215 $a1 online resource (11 pages) $cillustrations 225 1 $aNASA/TM ;$v2001-210396 300 $a"August 2001." 300 $a"Performing organization: NASA Dryden Flight Research Center"--Report documentation page. 320 $aIncludes bibliographical references (page 11). 606 $aX-33 reusable launch vehicle$2nasat 606 $aConfiguration management$2nasat 606 $aControl systems design$2nasat 606 $aFlight envelopes$2nasat 606 $aFlight control$2nasat 606 $aControl theory$2nasat 615 7$aX-33 reusable launch vehicle. 615 7$aConfiguration management. 615 7$aControl systems design. 615 7$aFlight envelopes. 615 7$aFlight control. 615 7$aControl theory. 700 $aCotting$b M. Christopher$01398018 702 $aBurken$b John J. 712 02$aNASA Dryden Flight Research Center, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCO 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910706591203321 996 $aReconfigurable control design for the full X-33 flight envelope$93460519 997 $aUNINA