Placement Optimization of Smart Piezoelectric Rods for Shape Control of Large Cable-Network Antenna Structures

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Large cable-network antennas are typical flexible space structures, which will inevitably generate deformations under various disturbances from out space. To avoid the degradation of shape accuracy due to deformations, it is imperative to find effective approaches to implement shape control for such antennas. In this paper, a novel application of smart piezoelectric rods that are mounted in the ring truss supporting structure of the antenna is presented to solve the shape control problem. The control mechanism is to generate displacements in opposite direction to resist primal deformations by using the direct piezoelectric effect of piezoceramic materials. Based on the genetic algorithm, optimal locations of the smart piezoelectric rods used for shape control is analyzed in the study. Numerical results demonstrate that the present shape control approach with appropriate placement of smart piezoelectric rods is feasible and effective.

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602-608

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June 2013

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© 2013 Trans Tech Publications Ltd. All Rights Reserved

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[1] M.W. Thomson, AstroMesh™ deployable reflectors for Ku- and Ka- band commercial satellites, Proc. 20th AIAA ICSSCE, AIAA-2002-2032 (2002).

DOI: 10.2514/6.2002-2032

Google Scholar

[2] A.G. Tibert, S. Pellegrino, Deployable tensegrity reflectors for small satellites, J. Spacecraft Rockets, 39(5) (2002) 701-709.

DOI: 10.2514/2.3867

Google Scholar

[3] A. Meguro, S. Harada, M. Watanabe, Key technologies for high accuracy large mesh antenna reflectors, Acta Astronaut. 53 (2003) 899-908.

DOI: 10.1016/s0094-5765(02)00211-4

Google Scholar

[4] Q. Chen, D. Natale, K. Ren, et al., Piezoelectric polymers actuators for precise shape control of large scale space antennas, Proc. SPIE 6524 (2007) 65241P1-65241P11.

DOI: 10.1117/12.717696

Google Scholar

[5] H. Furuya, Shape control of damaged space truss structures using genetic algorithms, AIAA Paper 96-1284 (1996) 399-405.

DOI: 10.2514/6.1996-1284

Google Scholar

[6] E.H. Anderson, et al., Development of an active truss element for control of precision structures, Optical Eng. 29(11) (1990) 1333-1341.

DOI: 10.1117/12.55735

Google Scholar

[7] Y.J. Yan, L.H. Yam, Optimal design of number and locations of actuators in active vibration control of a space truss, Smart Mater. Struct. 11 (2002) 496-503.

DOI: 10.1088/0964-1726/11/4/303

Google Scholar

[8] R.A. Burdisso, R.T. Haftka, Optimal location of actuators for correcting distortions in large truss structures, AIAA J. 27(10) (1989) 1406-1411.

DOI: 10.2514/3.10278

Google Scholar

[9] C.Y.K. Chee, et al., A review on the modelling of piezoelectric sensors and actuators incorporated in intelligent structures, J. Intell. Mater. Syst. Struct. 9 (1998) 3-19.

Google Scholar

[10] D.X. Li, W. Liu, J.P. Jiang, R. Xu, Placement optimization of actuator and sensor and decentralized adaptive fuzzy vibration control for large space intelligent truss structure, Sci. China Tech. Sci. 54 (2011) 853-861.

DOI: 10.1007/s11431-011-4333-0

Google Scholar