journal article·2020-09-20Open access

Structural Dynamic Improvement for Petal-Type Deployable Solid-Surface Reflector Based on Numerical Parameter Study

He Huang, Qiang Cheng, Lei Zheng

Applied Sciences· Volume 10· Issue 18

Abstract

Petal-type Deployable Solid-surface Reflector (PDSR) is a kind of important structure widely applied in deployable reflector antennas in aerospace engineering. The dynamic properties of this reflector structure in deployed state are significant to the reflector accuracy for antennas. However, the study of the dynamic evaluation of deployable structure with revolute joints is difficult and seldom concerned by researchers. In order to study dynamic properties of the PDSR, the Cable Replacement Method (CRM) was utilized to equivalently simulate the nonlinear structural stiffness of the revolute joint for numerical analyses. The Finite Element Model (FEM) of this reflector structure was established by commercial software ANSYS (ANSYS Inc., Canonsburg, PA, USA) and verified by the theoretical analysis and dynamic test of actual prototype model. The natural frequencies and mode shapes of deployed reflector were computed to study the influence of drag spring design parameters as stiffness, pre-tensioned force, and distance of two adjacent linkage butts. Finally, the analysis results were concluded that the drag springs between two adjacent petals can essentially improve the dynamic performance of reflector structure in deployed state. It can be a useful technical system for future engineering applications of PDSR antennas.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Structural Analysis and Optimization · Advanced Materials and Mechanics · Modular Robots and Swarm Intelligence

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi’an 710072, China

Funding

National Natural Science Foundation of China · Fundamental Research Funds for the Central Universities

References (29)

Show source-provided references
1. Technologies of large deployable space antennas
2. Research actuality and prospect of structure for space deployable antenna
3. Review of space deployable antenna mechanisms
4. Im, E., Thomson, M., Fang, H., Pearson, J., Moore, J., and Lin, J. (2007, January 18–20). Prospects of large deployable reflector antennas for a new generation of geostationary Doppler weather radar satellites. Proceedings of the AIAA, SPACE 2007 Conference & Exposition, Long Beach, CA, USA.10.2514/6.2007-9917 ↗
5. Semler, D., Tulintseff, A., Sorrell, R., and Marshburn, J. (September, January 30). Design, integration and deployment of the terreStar 18-meter reflector. Proceedings of the AIAA, 28th International Communications Satellite Systems Conference (ICSSC-2010), Anahelm, CA, USA.10.2514/6.2010-8855 ↗
6. Detection of open water dynamics with ENVISAT ASAR in support of land surface modelling at high latitudes10.5194/bg-9-703-2012 ↗
7. “RadioAstron”—A telescope with a size of 300000 km: Main parameters and first observational results10.1134/S1063772913030025 ↗
8. Advances and trends in space truss deployable antennae
9. Hoang, B., Spence, B., White, S., Spence, B., and Kiefer, S. (2016, January 5–12). Commercialization of deployable space systems’ roll-out solar array (ROSA) technology for Space Systems Loral (SSL) solar arrays. Proceedings of the 2016 IEEE Aerospace Conference, Big Sky, MT, USA.10.1109/AERO.2016.7500723 ↗
10. Deployment dynamics and control of large-scale flexible solar array system with deployable mast10.1016/j.asr.2016.06.008 ↗
11. Characteristics of the large deployable antenna on HALCA satellite in orbit10.1109/TAP.2004.831281 ↗
12. Deployable mast for solar sails in the range of 100–1000m10.1016/j.asr.2011.01.014 ↗
13. Design and deploying study of a new petal-type deployable solid surface antenna10.1016/j.actaastro.2018.04.042 ↗
14. Nonlinear dynamics and control of large deployable space structures composed of trusses and meshes
15. Structural optimization and model fabrication of a double-ring deployable antenna truss10.1016/j.actaastro.2013.10.002 ↗
16. Experimental studies of behavior of nonlinear dynamics of a deployable structure for spacecraft
17. Effects of joint on dynamics of space deployable structure10.3901/CJME.2013.05.861 ↗
18. Dynamic analysis of a deployable space structure10.2514/3.25090 ↗
19. Dynamic characteristics analysis of deployable space structures considering joint clearance10.1016/j.actaastro.2010.08.039 ↗
20. Structural design and optimization of large cable-rib tension deployable antenna structure with dynamic constraint10.1016/j.actaastro.2018.05.055 ↗
21. Wild, W., Baryshev, A., de Graauw, T., Kardashev, N., Likhachev, S., Goltsman, G., and Koshelets, V. (2008, January 28–30). Instrumentation for Millimetron—A large space antenna for THz astronomy. Proceedings of the International Symposium on Space Terahertz Technology, Groningen, The Netherlands.
22. Lee, J.Y., Yoon, S.S., Kim, S.H., Lee, T.K., Lee, J.W., Roh, J.H., and Yi, D.W. (2016, January 21–25). Performance of solid surface deployable antenna for panel misalignment. Proceedings of the 2016 URSI Asia-Pacific Radio Science Conference, Seoul, Korea.10.1109/URSIAP-RASC.2016.7601239 ↗
23. New Design of Petal Type Deployable Space Mirror10.1007/978-3-319-09858-6_37 ↗
24. Schwarz, S., and Barho, R. (2019, January 18–20). Deployment mechanisms for a 5m unfurlable reflector. Proceedings of the European Space Mechanisms and Tribology Symposium, Munich, Germany.
25. Mechanical study on initial profile solution for inflatable reflector made of orthotropic material10.1016/j.actaastro.2014.08.002 ↗
26. Huang, H., and Guan, F. (2019). Sensitivity Study on Optimizing Thickness Distribution for a Membrane Reflector. Int. J. Aerosp. Eng., 2019.10.1155/2019/3768746 ↗
27. Zhu, S. (2015). Design and Test of Deployable Plane Structure for Spaceborne Platform. [Master’s Thesis, Zhejiang University].
28. Clough, R.W., and Penzien, J. (2003). Dynamic of Structures, Computers & Structures, Inc.. [3rd ed.].
29. Jiangsu Donghua Test Technology Co. Ltd. (2020). Structural Mode Test. Analysis System Scheme, Jiangsu Donghua Test Technology Co. Ltd.. Technical Report No. DHC/J0.6-28.