001442275 000__ 03421cam\a2200565\i\4500
001442275 001__ 1442275
001442275 003__ OCoLC
001442275 005__ 20230310003321.0
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001442275 007__ cr\un\nnnunnun
001442275 008__ 210918s2022\\\\si\a\\\\ob\\\\000\0\eng\d
001442275 019__ $$a1287768573
001442275 020__ $$a9789811650970$$q(electronic bk.)
001442275 020__ $$a9811650977$$q(electronic bk.)
001442275 020__ $$z9789811650963
001442275 020__ $$z9811650969
001442275 0247_ $$a10.1007/978-981-16-5097-0$$2doi
001442275 035__ $$aSP(OCoLC)1268360722
001442275 040__ $$aYDX$$beng$$erda$$epn$$cYDX$$dGW5XE$$dOCLCO$$dOCLCF$$dDCT$$dOCLCQ$$dOCLCO$$dOCLCQ
001442275 049__ $$aISEA
001442275 050_4 $$aTL3260$$b.W36 2022
001442275 08204 $$a629.47/42$$223
001442275 1001_ $$aWang, Jie,$$eauthor.
001442275 24510 $$aRigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters /$$cJie Wang, Dong-Xu Li.
001442275 264_1 $$aSingapore :$$bSpringer,$$c[2022]
001442275 264_4 $$c©2022
001442275 300__ $$a1 online resource :$$billustrations (some color)
001442275 336__ $$atext$$btxt$$2rdacontent
001442275 337__ $$acomputer$$bc$$2rdamedia
001442275 338__ $$aonline resource$$bcr$$2rdacarrier
001442275 347__ $$atext file
001442275 347__ $$bPDF
001442275 504__ $$aIncludes bibliographical references.
001442275 5050_ $$aIntroduction -- Modeling of Flexible Spacecraft with Time-varying Parameters -- Dynamic Analysis of Flexible Spacecraft with Time-varying Parameters -- Vibration Control Methods for Systems in Complex Mode Space -- Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft -- Coupling Control Method for Flexible Spacecraft -- Attitude Coupling Control Experiments -- Future.
001442275 506__ $$aAccess limited to authorized users.
001442275 520__ $$aThis book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters. The dynamic characteristics, vibration control methods and attitude stabilization methods for spacecraft are systematically studied in respects of the theoretical modeling, numerical simulation and the ground experiment. Three active control theories in complex mode space are presented for flexible space structures. Optimal slew strategies based on variable amplitudes input shaping methods and coupling control methods are proposed for stabilization of flexible spacecraft. The research provides an important way to solve the problem of high-precision attitude control of flexible spacecraft with time-varying parameters. This book is appropriate for the researchers who focus on the multi-body dynamics, attitude and vibration control of flexible spacecraft.
001442275 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed September 23, 2021).
001442275 650_0 $$aSpace vehicles$$xAttitude control systems.
001442275 650_0 $$aStability of space vehicles.
001442275 650_6 $$aVéhicules spatiaux$$xSystèmes de commande d'orientation.
001442275 650_6 $$aVaisseaux spatiaux$$xStabilité.
001442275 655_0 $$aElectronic books.
001442275 7001_ $$aLi, Dong-Xu,$$eauthor.
001442275 77608 $$iPrint version:$$aWang, Jie.$$tRigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters.$$dSingapore : Springer, [2022]$$z9811650969$$z9789811650963$$w(OCoLC)1259046180
001442275 852__ $$bebk
001442275 85640 $$3Springer Nature$$uhttps://univsouthin.idm.oclc.org/login?url=https://link.springer.com/10.1007/978-981-16-5097-0$$zOnline Access$$91397441.1
001442275 909CO $$ooai:library.usi.edu:1442275$$pGLOBAL_SET
001442275 980__ $$aBIB
001442275 980__ $$aEBOOK
001442275 982__ $$aEbook
001442275 983__ $$aOnline
001442275 994__ $$a92$$bISE