LEADER 01536nam0 22003131i 450 001 UON00264409 005 20231205103727.406 010 $a96-461-8909-1 100 $a20050530d1997 |0itac50 ba 101 $aira 102 $aIR 105 $a|||| 1|||| 200 1 $aAsnadi ahzab-e siyasi-e Iran: 1320-1330 Sh. / bih kushish-e Bihruz Tayarani 205 $aTehran : Sazman-e Asnad-e Milli-e Iran$b1374 [1997] 210 $a2 v.$cill. ; 25 cm 215 $aAltro front.$cPolitical parties in Iran. A collection of Documents (1941-1951) / by Behrouz Tayarani 316 $aAltro inv. 113585$5IT-UONSI IRAVB/011 (1) N 510 1$3UON00374490$aPolitical parties in Iran a collection of documents (1941-1951) / B. Tayarani 606 $aIran$xPolitica e governo$xSec. 20.$3UONC021190$2FI 620 $aIR$dTihra?n$3UONL005570 686 $aIRA V B$cIRAN - POLITOLOGIA - MOVIMENTI POLITICI E SINDACALI$2A 700 1$aTAYARANI$bBehrouz$3UONV153953$0690149 712 $aSazman-e asnad-e melli-e Iran$3UONV250911$4650 801 $aIT$bSOL$c20250606$gRICA 912 $aUON00264409 950 $aSIBA - SISTEMA BIBLIOTECARIO DI ATENEO$dSI IRA V B 011 (1) N $eSI SA 113584 7 011 (1) N Altro inv. 113585 950 $aSIBA - SISTEMA BIBLIOTECARIO DI ATENEO$dSI IRA V B 011 (2) N $eSI SA 113585 7 011 (2) N 996 $aAsnadi ahzab-e siyasi-e Iran: 1320-1330 Sh$91241077 997 $aUNIOR LEADER 03165nam 22006015 450 001 9910627239003321 005 20251009075105.0 010 $a981-19-4637-X 024 7 $a10.1007/978-981-19-4637-0 035 $a(CKB)5840000000091768 035 $a(MiAaPQ)EBC7101864 035 $a(Au-PeEL)EBL7101864 035 $a(PPN)264957741 035 $a(DE-He213)978-981-19-4637-0 035 $a(OCoLC)1347029192 035 $a(EXLCZ)995840000000091768 100 $a20220922d2023 u| 0 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aRedundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle /$fby Xuefeng Li, Fan Xu, Guoqiang Xu 205 $a1st ed. 2023. 210 1$aSingapore :$cSpringer Nature Singapore :$cImprint: Springer,$d2023. 215 $a1 online resource (196 pages) 225 1 $aNavigation: Science and Technology,$x2522-0462 ;$v12 311 08$a981-19-4636-1 320 $aIncludes bibliographical references and index. 327 $aSection 1 Introduction -- Section 2 Model of Launch Vehicle Dynamics and Redundant Strapdown IMUs -- Section 3 Redundant IMU Fault Detection -- Section 4 Redundant IMU Reconfiguration -- Section 5 Trajectory Replanning. 330 $aThis book analyzes the problems to be solved urgently in the development of launch vehicle control system. The techniques of redundant Inertial Measurement Unit (IMU) reconfiguration and trajectory replanning are proposed aiming at the inertial device failures and power system failures during flight of launch vehicles, respectively. It introduces the background of redundant IMU reconfiguration and trajectory replanning technologies and models of launch vehicle dynamics and redundant strap-down IMUs. The approaches for redundant strap-down IMU fault detection, reconfiguration and trajectory replanning are proposed, putting forward a prospect for the development of launch vehicle control system. The content of this book is concise and highly pragmatic. It could serve as a reference for engineers and researchers engaged in the analysis, design and verification of launch vehicle control systems and also as a reference for graduate students and senior undergraduates majoring in navigation,guidance and control. 410 0$aNavigation: Science and Technology,$x2522-0462 ;$v12 606 $aAerospace engineering 606 $aAstronautics 606 $aEngines 606 $aAerospace Technology and Astronautics 606 $aEngine Technology 615 0$aAerospace engineering. 615 0$aAstronautics. 615 0$aEngines. 615 14$aAerospace Technology and Astronautics. 615 24$aEngine Technology. 676 $a531.12 700 $aLi$b Xuefeng$01062277 702 $aXu$b Guoqiang 702 $aXu$b Fan 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910627239003321 996 $aRedundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle$92975418 997 $aUNINA