LEADER 03413nam  22006735  450 
001 9910743364903321
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010   $a981-16-5097-7
010   $a981-16-5096-9
010   $a981-16-5097-7
024 7 $a10.1007/978-981-16-5097-0
035   $a(CKB)4100000012027026
035   $a(MiAaPQ)EBC6727842
035   $a(Au-PeEL)EBL6727842
035   $a(OCoLC)1273979221
035   $a(PPN)258058463
035   $a(DE-He213)978-981-16-5097-0
035   $a(EXLCZ)994100000012027026
100   $a20210915d2022      u|         0
101 0 $aeng
135   $aurcnu||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aRigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters /$fby Jie Wang, Dong-Xu Li
205   $a1st ed. 2022.
210  1$aSingapore :$cSpringer Nature Singapore :$cImprint: Springer,$d2022.
215   $a1 online resource (190 pages)
225 1 $aIntelligent Technologies and Robotics Series
311 08$a981-16-5096-9 
327   $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.
330   $aThis book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters. The dynamic characteristics, vibration control methods and attitude stabilization methods for spacecraft are systematically studied in respects of the theoretical modeling, numerical simulation and the ground experiment. Three active control theories in complex mode space are presented for flexible space structures. Optimal slew strategies based on variable amplitudes input shaping methods and coupling control methods are proposed for stabilization of flexible spacecraft. The research provides an important way to solve the problem of high-precision attitude control of flexible spacecraft with time-varying parameters. This book is appropriate for the researchers who focus on the multi-body dynamics, attitude and vibration control of flexible spacecraft.
410  0$aIntelligent Technologies and Robotics Series
606   $aAutomatic control
606   $aDynamics
606   $aNonlinear theories
606   $aAerospace engineering
606   $aAstronautics
606   $aControl and Systems Theory
606   $aApplied Dynamical Systems
606   $aAerospace Technology and Astronautics
615  0$aAutomatic control.
615  0$aDynamics.
615  0$aNonlinear theories.
615  0$aAerospace engineering.
615  0$aAstronautics.
615 14$aControl and Systems Theory.
615 24$aApplied Dynamical Systems.
615 24$aAerospace Technology and Astronautics.
676   $a629.4742
700   $aWang$b Jie$f1275-1336,$01427387
702   $aLi$b Dong-Xu
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910743364903321
996   $aRigid-flexible coupling dynamics and control of flexible spacecraft with time-varying parameters$93560476
997   $aUNINA