LEADER 00983nam0-22003131i-450- 001 990007074460403321 005 20061019123132.0 010 $a88-222-4844-9 035 $a000707446 035 $aFED01000707446 035 $a(Aleph)000707446FED01 035 $a000707446 100 $a20020422d2000----km-y0itay50------ba 101 0 $aita 105 $ay-------001yy 200 1 $aBenvenuto Olivieri$ei mercatores fiorentini e la Camera Apostolica nella Roma di Paolo III Farnese$e(1534-1549)$fFrancesco Guidi Bruscoli 210 $aFirenze$cOlschki$d2000 215 $a362 p.$d24 cm 225 1 $aQuaderni$fFondazione Carlo Marchi$v6 610 0 $aBANCHIERI. FIRENZE. FAMIGLIA OLIVIERI. 1534-1549 676 $a332.1092$v21$zita 700 1$aGuidi Bruscoli,$bFrancesco$0260226 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990007074460403321 952 $a332.1 GUI 1$fFLFBC 959 $aFLFBC 996 $aBenvenuto Olivieri$9705984 997 $aUNINA LEADER 02811nam 2200613 a 450 001 9910781405103321 005 20230307052039.0 010 $a1-60086-722-7 035 $a(CKB)2550000000072649 035 $a(CtWfDGI)bke00043379 035 $a(SSID)ssj0000550919 035 $a(PQKBManifestationID)12207220 035 $a(PQKBTitleCode)TC0000550919 035 $a(PQKBWorkID)10524945 035 $a(PQKB)10693397 035 $a(Au-PeEL)EBL3111684 035 $a(CaPaEBR)ebr10516789 035 $a(OCoLC)922979132 035 $a(MiAaPQ)EBC3111684 035 $a(EXLCZ)992550000000072649 100 $a20090821d2009 uy 0 101 0 $aeng 135 $aurzn|||||| 181 $ctxt 182 $cc 183 $acr 200 10$aAnalytical mechanics of space systems /$fHanspeter Schaub, John L. Junkins 205 $a2nd edition. 210 $aReston, Va. $cAmerican Institute of Aeronautics and Astronautics$dc2009 215 $axxi, 793 p. $cill 225 1 $aAIAA education series 300 $aTitle from title screen. 311 $a1-60086-721-9 320 $aIncludes bibliographical references and index. 327 $aParticle kinematics -- Newtonian mechanics -- Rigid body kinematics -- Eulerian mechanics -- Generalized methods of analytical dynamics -- Variational methods in analytical dynamics -- Hamilton's generalized formulations of analytical dynamics -- Nonlinear spacecraft stability and control -- Classical two-body problem -- Restricted three-body problem -- Gravitational potential field models -- Perturbation methods -- Transfer orbits -- Spacecraft formation flying -- Appendix A. Transport theorem derivation using linear algebra -- Appendix B. Various Euler angle transformations -- Appendix C. MRP identity proof -- Appendix D. Conic section transformations -- Appendix E. Numerical subroutines library -- Appendix F. First-order mapping between mean and osculating orbit elements -- Appendix G. Direct linear mapping between Cartesian Hill frame coordinates and orbit element differences -- Appendix H. Hamel coefficients for the rotational motion of a rigid body. 410 0$aAIAA education series. 606 $aCelestial mechanics 606 $aDifferentiable dynamical systems 606 $aOrbital mechanics 606 $aSpace vehicles$xControl systems 615 0$aCelestial mechanics. 615 0$aDifferentiable dynamical systems. 615 0$aOrbital mechanics. 615 0$aSpace vehicles$xControl systems. 676 $a521 700 $aSchaub$b Hanspeter$01513838 701 $aJunkins$b John L$08527 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910781405103321 996 $aAnalytical mechanics of space systems$93748496 997 $aUNINA