摘要
The surface precision of an antenna reflector can be improved using the actuation of piezoelectric materials to obtain a high-performance space antenna. In this study, the active shape control of a reflector with piezoceramic (lead zirconate titanate) actuators assembled on ribs is proposed by theoretical and experimental approaches. A finite element model of the integrated reflector–actuator system is established using piezoelectric constitutive equations and the virtual work’s principle. For a desired shape, a closed-loop iterative shape control method based on the influence coefficient matrix model is developed, which resolves the issue of high-precision shape control of the antenna reflector in the presence of model errors. The shape controller based on the proposed closed-loop shape control method is implemented on a planar hexagonal reflector with 30 lead zirconate titanate actuators. Experimental results demonstrate that the closed-loop control is an effective way to improve the surface precision of the reflector considering uncertainties.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 2733-2747 |
| 页数 | 15 |
| 期刊 | Journal of Intelligent Material Systems and Structures |
| 卷 | 30 |
| 期 | 18-19 |
| DOI | |
| 出版状态 | 已出版 - 1 11月 2019 |
| 已对外发布 | 是 |
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