LEADER 05206nam 2200685 450 001 9910826042303321 005 20230808192256.0 010 $a1-119-01561-8 010 $a1-119-01560-X 035 $a(CKB)3710000000621175 035 $a(EBL)4454415 035 $a(OCoLC)945613365 035 $a(SSID)ssj0001635546 035 $a(PQKBManifestationID)16389360 035 $a(PQKBTitleCode)TC0001635546 035 $a(PQKBWorkID)14950548 035 $a(PQKB)10564676 035 $a(PQKBManifestationID)16394025 035 $a(PQKB)23562992 035 $a(MiAaPQ)EBC4454415 035 $a(DLC) 2015035137 035 $a(Au-PeEL)EBL4454415 035 $a(CaPaEBR)ebr11175910 035 $a(CaONFJC)MIL909321 035 $a(EXLCZ)993710000000621175 100 $a20160413h20162016 uy 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt 182 $cc 183 $acr 200 10$aFlexible multibody dynamics $eefficient formulations and applications /$fArun K. Banerjee 210 1$aWest Sussex, England :$cWiley,$d2016. 210 4$dİ2016 215 $a1 online resource (339 p.) 300 $aDescription based upon print version of record. 311 $a1-119-01563-4 311 $a1-119-01564-2 320 $aIncludes bibliographical references and index. 327 $aTitle Page; Copyright; Dedication; Preface; 1 Derivation of Equations of Motion; 1.1 Available Analytical Methods and the Reason for Choosing Kane's Method; 1.2 Kane's Method of Deriving Equations of Motion; 1.3 Comparison to Derivation of Equations of Motion by Lagrange's Method; 1.4 Kane's Method of Direct Derivation of Linearized Dynamical Equation; 1.5 Prematurely Linearized Equations and a Posteriori Correction by ad hoc Addition of Geometric Stiffness due to Inertia Loads; 1.6 Kane's Equations with Undetermined Multipliers for Constrained Motion 327 $a1.7 Summary of the Equations of Motion with Undetermined Multipliers for Constraints 1.8 A Simple Application; Appendix 1. A Guidelines for Choosing Efficient Motion Variables in Kane's Method; Problem Set 1; References; 2 Deployment, Station-Keeping, and Retrieval of a Flexible Tether Connecting a Satellite to the Shuttle; 2.1 Equations of Motion of a Tethered Satellite Deployment from the Space Shuttle; 2.2 Thruster-Augmented Retrieval of a Tethered Satellite to the Orbiting Shuttle; 2.3 Dynamics and Control of Station-Keeping of the Shuttle-Tethered Satellite 327 $aAppendix 2.A Sliding Impact of a Nose Cap with a Package of Parachute Used for Recovery of a Booster Launching Satellites Appendix 2.B Formation Flying with Multiple Tethered Satellites; Appendix 2.C Orbit Boosting of Tethered Satellite Systems by Electrodynamic Forces; Problem Set 2; References; 3 Kane's Method of Linearization Applied to the Dynamics of a Beam in Large Overall Motion; 3.1 Nonlinear Beam Kinematics with Neutral Axis Stretch, Shear, and Torsion; 3.2 Nonlinear Partial Velocities and Partial Angular Velocities for Correct Linearization 327 $a3.3 Use of Kane's Method for Direct Derivation of Linearized Dynamical Equations 3.4 Simulation Results for a Space-Based Robotic Manipulator; 3.5 Erroneous Results Obtained Using Vibration Modes in Conventional Analysis; Problem Set 3; References; 4 Dynamics of a Plate in Large Overall Motion; 4.1 Motivating Results of a Simulation; 4.2 Application of Kane's Methodology for Proper Linearization; 4.3 Simulation Algorithm; 4.4 Conclusion; Appendix 4.A Specialized Modal Integrals; Problem Set 4; References; 5 Dynamics of an Arbitrary Flexible Body in Large Overall Motion 327 $a5.1 Dynamical Equations with the Use of Vibration Modes 5.2 Compensating for Premature Linearization by Geometric Stiffness due to Inertia Loads; 5.3 Summary of the Algorithm; 5.4 Crucial Test and Validation of the Theory in Application; Appendix 5.A Modal Integrals for an Arbitrary Flexible Body [2]; Problem Set 5; References; 6 Flexible Multibody Dynamics: Dense Matrix Formulation; 6.1 Flexible Body System in a Tree Topology; 6.2 Kinematics of a Joint in a Flexible Multibody Body System; 6.3 Kinematics and Generalized Inertia Forces for a Flexible Multibody System 327 $a6.4 Kinematical Recurrence Relations Pertaining to a Body and Its Inboard Body 330 $a"This book describes how to build mathematical models of multibody systems with elastic components. Examples of such systems are the human body itself, construction cranes, cars with trailers, helicopters, spacecraft deploying antennas, tethered satellites, and underwater maneuvering vehicles looking for mines while being connected by a cable to a ship"--$cProvided by publisher. 606 $aMachinery, Dynamics of 606 $aMultibody systems$xMathematical models 615 0$aMachinery, Dynamics of. 615 0$aMultibody systems$xMathematical models. 676 $a621.8/11 686 $aTEC009070$2bisacsh 700 $aBanerjee$b Arun K.$01593676 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910826042303321 996 $aFlexible multibody dynamics$93913924 997 $aUNINA