Flexible actuator finite element applied to spatial mechanisms by a finite deformation dynamic formulation-Reference-Cited by-同舟云学术

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Flexible actuator finite element applied to spatial mechanisms by a finite deformation dynamic formulation

Published:2019-05-31 Issue:6 Volume:64 Page:1517-1535
ISSN:0178-7675
Container-title:Computational Mechanics
language:en
Short-container-title:Comput Mech

Author:

Siqueira Tiago Morkis^ORCID,Coda Humberto Breves

Funder

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior

Fundação de Amparo à Pesquisa do Estado de São Paulo

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,Computational Mathematics,Computational Theory and Mathematics,Mechanical Engineering,Ocean Engineering,Computational Mechanics

Link

http://link.springer.com/content/pdf/10.1007/s00466-019-01732-0.pdf

Reference45 articles.

1. Coda HB, Paccola RR (2011) A FEM procedure based on positions and unconstrained vectors applied to non-linear dynamic of 3D frames. Finite Elem Anal Des 47:319–333

2. Coda HB, Paccola RR, Sampaio MDSM (2013) Positional description applied to the solution of geometrically non-linear plates and shells. Finite Elem Anal Des 67:66–75

3. Thomson MW (1999) The AstroMesh deployable reflector. In: IEEE antennas and propagation society international symposium: wireless technologies and information networks, APS 1999—Held in conjunction with USNC/URSI National Radio Science Meeting. IEEE, pp 1516–1519

4. Takano T, Miura K, Natori M et al (2004) Deployable antenna with 10-m maximum diameter for space use. IEEE Trans Antennas Propag 52:2–11. https://doi.org/10.1109/TAP.2003.820968

5. Meguro A, Shintate K, Usui M, Tsujihata A (2009) In-orbit deployment characteristics of large deployable antenna reflector onboard Engineering Test Satellite VIII. Acta Astronaut 65:1306–1316. https://doi.org/10.1016/j.actaastro.2009.03.052

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