Optimization Design of Cable-Frame Antennas Based on Tension Compensation Method

Article Preview

Abstract:

Tension truss reflectors are flexible structures characterized by strong geometric nonlinearities, thus the surface error and the real cable tensions of a reflector cannot be controlled efficiently to anticipant levels by their initial cable tensions. To ensure both appropriate node positions and anticipant cable tensions, an optimization method based on Tension Compensation Method is presented. First, a parameterized description of the zero-stress states of the front net and the rear net is proposed and the strategy of Tension Compensation Method is used to control the cable tensions to anticipant levels. Second, a mathematical optimization model for the cable tensions and the zero-stress state design of the cable network is established based on Tension Compensation Method with the optimization target of minimizing surface error of the reflector. Finally, the feasibility and effectiveness of the presented method are validated by some numerical examples. The results show that the cable tensions can be effectively controlled by the proposed method, and this method can generate regular zero-stress states of the cable-nets which may bring great convenience to the lofting work of the cable network.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

797-803

Citation:

Online since:

January 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] S. Dennis, T. Ann, S. Rodney, M. James, in: 28th AIAA International Communications Satellite Systems Conference, 2010, California.

Google Scholar

[2] K. Miura, Y. Miyazaki, AIAA Journal, Vol. 28, No. 6 (1990), pp.1098-1104.

Google Scholar

[3] H. Ken, K. Naoko, et al, in: 50th AIAA Structures, Structural Dynamics, and Materials Conference, 2009, California.

Google Scholar

[4] M. W. Thomson, in: IUTAM-IASS Symposium on Deployable Structures: Theory and Applications, Cambridge, UK, 6-9 September, (1998).

Google Scholar

[5] Z. You, S. Pellegrino, AIAA Journal, Vol. 35, No. 8 (1997), pp.1348-1355.

Google Scholar

[6] A.G. Tibert, in: 44th AIAA/ASME/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Norfolk, VA, 7-10 April 2003, AIAA-2003-1629.

DOI: 10.2514/6.2003-1978

Google Scholar

[7] G. Li, F. L. Guan, Acta Mechanica Solida Sinica, (2006) pp.174-179.

Google Scholar

[8] D.W. Yang, Y.Y. Qiu, H. Bao, Journal of Mechanical Engineering, Vol. 48, No. 21(2012), pp.22-27.

Google Scholar

[9] J.J. Di, in: 3rd International Symposium on Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010, Harbin, China.

Google Scholar

[10] R. Yang, Xi'an: Xidian University, (2010).

Google Scholar

[11] J.J. Di, B.Y. Duan, Y. Luo, Journal of South China University of Technology (Natural Science Edition), Vol. 32, No. 6 (2004), pp.23-26.

Google Scholar

[12] G.Q. You, J. Zhang, Engineering Mechanics, Vol. 29, No. 11(2012), p.306: 312.

Google Scholar

[13] M. Sebastien, M. Bernard, Q. Jerome, Acta Astronautica, Vol. 76(2012), pp.154-163.

Google Scholar

[14] X. Zhuo, Industrial Building, (2002), pp.310-316.

Google Scholar

[15] Y. Guo, Industrial Building, (2003), 343-347.

Google Scholar