LEADER 01066nam0-22003611i-450- 001 990008132780403321 005 20060711113744.0 010 $a88-220-4137-2 035 $a000813278 035 $aFED01000813278 035 $a(Aleph)000813278FED01 035 $a000813278 100 $a20050620d1989----km-y0itay50------ba 101 1 $aita 102 $aIT 105 $aa-------001yy 200 1 $a<>genesi di Noto$euna cittą siciliana del Settecento$fStephen Tobriner$gedizione italiana a cura di Corrado Latina 210 $aBari$cDedalo$d1989 215 $aXVI, 251 p.$cill.$d31 cm 454 0$12001$a<>genesis of Noto$954707 610 0 $aNoto$aEdilizia$aRicostruzione$aSec. 18. 610 0 $aTerremoti$aNoto$a1693 700 1$aTobriner,$bStephen$0287236 702 1$aLatina,$bCorrado 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990008132780403321 952 $aCI.02.078$b148$fCICE 952 $a17.023$b956$fDARST 959 $aCICE 959 $aDARST 996 $aGenesis of Noto$954707 997 $aUNINA LEADER 00743nam0-22002651i-450- 001 990001015350403321 035 $a000101535 035 $aFED01000101535 035 $a(Aleph)000101535FED01 035 $a000101535 100 $a--------d--------km-y0itay50------ba 101 0 $aeng 200 1 $a<>Introduction to Harmonic Analysis$fYitzhak Katznelson 210 $aNew York$cJohn Wiley$d1968 610 0 $aAnalisi funzionale 610 0 $aAlgebre astratte 676 $a517.00//517.36 700 1$aKatznelson,$bYitzhak$048154 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990001015350403321 952 $a14A-071$b6329$fFI1 959 $aFI1 996 $aIntroduction to harmonic analysis$985375 997 $aUNINA LEADER 02431oam 2200685I 450 001 9910713752503321 005 20200731105004.0 035 $a(CKB)5470000002504159 035 $a(OCoLC)1104148317 035 $a(EXLCZ)995470000002504159 100 $a20190610d1952 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAnalogue-computer simulation of an autopilot servo system having nonlinear response characteristics /$fby Arthur L. Jones and John S. White 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1952. 215 $a1 online resource (30 pages) $cillustrations 225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 2707 300 $a"June 1952." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 14). 606 $aAnalog computer simulation 606 $aAutomatic control 606 $aAutomatic pilot (Airplanes) 606 $aElectronic differential analyzers 606 $aNonlinear systems 606 $aServomechanisms 606 $aAnalog computer simulation$2fast 606 $aAutomatic control$2fast 606 $aAutomatic pilot (Airplanes)$2fast 606 $aElectronic differential analyzers$2fast 606 $aNonlinear systems$2fast 606 $aServomechanisms$2fast 615 0$aAnalog computer simulation. 615 0$aAutomatic control. 615 0$aAutomatic pilot (Airplanes) 615 0$aElectronic differential analyzers. 615 0$aNonlinear systems. 615 0$aServomechanisms. 615 7$aAnalog computer simulation. 615 7$aAutomatic control. 615 7$aAutomatic pilot (Airplanes) 615 7$aElectronic differential analyzers. 615 7$aNonlinear systems. 615 7$aServomechanisms. 700 $aJones$b Arthur L.$01413432 702 $aWhite$b John S. 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bTRAAL 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910713752503321 996 $aAnalogue-computer simulation of an autopilot servo system having nonlinear response characteristics$93509838 997 $aUNINA