Sanfedino, Francesco and Alazard, Daniel
and Pommier-Budinger, Valérie
and Falcoz, Alexandre and Boquet, Fabrice
Finite element based N-Port model for preliminary design of multibody systems.
(2018)
Journal of Sound and Vibration, 415. 128-146. ISSN 0022-460X
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(Document in English)
PDF (Author's version) - Requires a PDF viewer such as GSview, Xpdf or Adobe Acrobat Reader 3MB |
Official URL: https://doi.org/10.1016/j.jsv.2017.11.021
Abstract
This article presents and validates a general framework to build a linear dynamic Finite Element-based model of large exible structures for integrated Control/Structure design. An extension of the Two-Input Two-Output Port (TITOP) approach is here developed. The authors had already proposed such framework for simple beam-like structures: each beam was considered as a TITOP sub-system that could be interconnected to another beam thanks to the ports. The present work studies bodies with multiple attaching points by allowing complex interconnections among several sub-structures in tree-like assembly. The TITOP approach is extended to generate NINOP (N-Input N-Output Port) models. A Matlab toolbox is developed integrating beam and bending plate elements. In particular a NINOP formulation of bending plates is proposed to solve analytic twodimensional problems. The computation of NINOP models using the outputs of a MSC/Nastran modal analysis is also investigated in order to directly use the results provided by a commercial finite element software. The main advantage of this tool is to provide a model of a multibody system under the form of a block diagram with a minimal number of states. This model is easy to operate for preliminary design and control. An illustrative example highlights the potential of the proposed approach: the synthesis of the dynamical model of a spacecraft with two deployable and exible solar arrays.
Item Type: | Article |
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Additional Information: | Thanks to Elsevier editor. The original PDF of the article can be found at http://www.sciencedirect.com/science/article/pii/S0022460X17307915 |
Audience (journal): | International peer-reviewed journal |
Uncontrolled Keywords: | |
Institution: | Other partners > Airbus (FRANCE) Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE-SUPAERO (FRANCE) Other partners > ESA - ESTEC (NETHERLANDS) |
Laboratory name: | |
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Deposited On: | 19 Dec 2017 09:22 |
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