Finite Element Modeling and Modal Analysis of Coilable Mast

Author:

Wang Jie1,Li Dong Xu2,Jiang Jian Ping2

Affiliation:

1. National University of Defense Technology

2. National University of Defense Technology

Abstract

This paper investigates the modal characteristics of a coilable mast for space mission applications. Finite element models are established for characterizing the coilable mast. The simplification of joints between longerons and batten frames and the pre-tension in cables are carefully considered. A parametric modal analysis is performed with considering the following factors, the joint model in the truss, the pre-tension in cables, elements selected for longerons and battens, the mass attached to the top of the mast. Research results show that the natural frequencies of the coilable mast are sensitive to the selected elements and the attached mass. The pre-tension level in cables and the precision degree of the joint model have little effect on natural frequencies. The regularity expressed in the parametric modal analysis is useful for designers and engineers.

Publisher

Trans Tech Publications, Ltd.

Reference10 articles.

1. L. Puig, A. Barton and N. Rando: Acta Astronautica, Vol. 67(2010), p.12.

2. Y. Soucy, F.R. Vigneron: Proc. 25th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference (Palm Springs, California, May 14-16, 1984), p.130.

3. K.S. Carney, F.J. Shaker: Proc. 30th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference (Mobile, Alabama, April 3-5, 1989), p.812.

4. X. Zhou, G.N. Yue, H. Huang and X.S. Wang: Proc. 3rd International Symposium on Systems and Control in Aeronautics and Astronautics (Harbin, China, June 8-10, 2010), p.1329.

5. M.E. McEachen, T.A. Trautt and D.M. Murphy: Proc. 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (Austin, Texas, April 18-21, 2005).

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