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dc.contributor.authorArnold, Martin
dc.contributor.authorHante, Stefan
dc.date.accessioned2017-11-25T07:20:19Z
dc.date.available2017-11-25T07:20:19Z
dc.date.copyright2016/2/12
dc.date.issued2017
dc.identifier.issn1555-1415
dc.identifier.othercnd_012_02_021002.pdf
dc.identifier.urihttp://138.201.223.254:8080/yetl1/handle/yetl/4236366
dc.description.abstractConfiguration spaces with Lie group structure display kinematical nonlinearities of mechanical systems. In Lie group time integration, this nonlinear structure is also considered at the time-discrete level using nonlinear updates of the configuration variables. For practical implementation purposes, these update formulae have to be adapted to each specific Lie group setting that may be characterized from the algorithmic viewpoint by group operation, exponential map, tilde, and tangent operator. In this paper, we discuss these practical aspects for the time integration of a geometrically exact Cosserat rod model with rotational degrees-of-freedom being represented by unit quaternions. Shearing and longitudinal extension of the Cosserat rod may be neglected using suitable constraints that result in a differential-algebraic equation (DAE) formulation of the beam structure. The specific structure of unconstrained systems and constrained systems is exploited by tailored algorithms for the corrector iteration of the generalized-α Lie group integrator.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleImplementation Details of a Generalized-α Differential-Algebraic Equation Lie Group Method
dc.typeJournal Paper
dc.journal.volume12
dc.journal.issue2
dc.journal.titleJournal of Computational and Nonlinear Dynamics
dc.identifier.doi10.1115/1.4033441
dc.journal.fristpage21002
dc.journal.lastpage021002-8
dc.treeJournal of Computational and Nonlinear Dynamics:;2017:;volume( 012 ):;issue: 002
dc.contenttypeFulltext


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