2016
DOI: 10.1007/s11044-016-9559-y
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Linear dynamics of flexible multibody systems

Abstract: We present a new methodology to derive a linear model of flexible multibody system dynamics. This approach is based on the two-port model of each body allowing the model of the whole system to be built just connecting the inputs/outputs of each body model. Boundary conditions of each body can be taken into account through inversion of some input-output channels of its two-port model. This approach is extended here to treat the case of closed-loop kinematic mechanisms. Lagrange multipliers are commonly used in … Show more

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Cited by 26 publications
(45 citation statements)
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“…This first assumption does not constrain the dynamic analysis to the clamped-free condition as already demonstrated in Ref. [33] for an homogeneous beam, but it allows simplifying Eq. (7) without any loss of information and studying any kind of boundary conditions.…”
Section: The Titop Approachmentioning
confidence: 99%
See 3 more Smart Citations
“…This first assumption does not constrain the dynamic analysis to the clamped-free condition as already demonstrated in Ref. [33] for an homogeneous beam, but it allows simplifying Eq. (7) without any loss of information and studying any kind of boundary conditions.…”
Section: The Titop Approachmentioning
confidence: 99%
“…(6) (13) This model, conceived with the clamped-free condition, is useful to study any other kind of boundary configuration as proved in Ref. [33] thanks to the invertibility of all of its 12 input-output channels. Moreover the TITOP model allows us to directly link several sub-structures of an open/closed chain-like complex body.…”
Section: The Titop Approachmentioning
confidence: 99%
See 2 more Smart Citations
“…The advantage of this method is to be modular and appropriate for control/structure co-design. The TITOP approach is applied in [4] to study any flexible multi-body system with closed-loop kinematic chains and in [5] to model flexible solar panels considered as bending plates connected to a spacecraft main body.…”
Section: Introductionmentioning
confidence: 99%