Active shape control of an antenna reflector using piezoelectric actuators
Source abstract
Abstract
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.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Structural Analysis and Optimization · Aeroelasticity and Vibration Control · Composite Structure Analysis and Optimization
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
School of Aeronautics and Astronautics, Dalian University of Technology, Dalian, China
State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian, China
Funding
National Natural Science Foundation of China · fundamental research funds for the central universities
References (32)
Show source-provided references
1. 10.1088/0964-1726/8/6/30310.1088/0964-1726/8/6/303 ↗
2. 10.1002/nme.162002020210.1002/nme.1620020202 ↗
3. 10.2514/3.2002910.2514/3.20029 ↗
4. 10.2514/6.2013-152510.2514/6.2013-1525 ↗
5. 10.2514/2.156110.2514/2.1561 ↗
6. 10.1016/S0045-7825(99)00265-010.1016/S0045-7825(99)00265-0 ↗
7. Datashvili L · 2010 · 1
8. 10.2514/1.2510910.2514/1.25109 ↗
9. 10.1117/12.27569310.1117/12.275693 ↗
10. 10.1088/0964-1726/22/12/12503210.1088/0964-1726/22/12/125032 ↗
11. 10.1106/HYTV-NC7R-BCMM-W3CH10.1106/HYTV-NC7R-BCMM-W3CH ↗
12. 10.1364/AO.52.00236310.1364/AO.52.002363 ↗
13. 10.2514/1.A3223110.2514/1.A32231 ↗
14. 10.1016/S0141-0296(01)00081-510.1016/S0141-0296(01)00081-5 ↗
15. 10.1016/j.actaastro.2010.07.01710.1016/j.actaastro.2010.07.017 ↗
16. 10.1088/0964-1726/22/9/09501310.1088/0964-1726/22/9/095013 ↗
17. Lan L · 2016 · 9799
18. 10.1016/S0022-460X(03)00110-X10.1016/S0022-460X(03)00110-X ↗
19. 10.1007/s12567-013-0048-310.1007/s12567-013-0048-3 ↗
20. 10.1088/1361-665X/aad48010.1088/1361-665X/aad480 ↗
21. 10.1088/0964-1726/25/12/12501810.1088/0964-1726/25/12/125018 ↗
22. 10.1016/j.actaastro.2010.09.02510.1016/j.actaastro.2010.09.025 ↗
23. 10.2514/2.57310.2514/2.573 ↗
24. 10.1016/j.compstruc.2006.01.02610.1016/j.compstruc.2006.01.026 ↗
25. 10.1016/S0168-874X(97)00086-310.1016/S0168-874X(97)00086-3 ↗
26. 10.1016/j.compstruct.2018.05.06010.1016/j.compstruct.2018.05.060 ↗
27. 10.1243/09544100JAERO39410.1243/09544100JAERO394 ↗
28. 10.1061/(ASCE)AS.1943-5525.000085810.1061/(ASCE)AS.1943-5525.0000858 ↗
29. 10.1088/0964-1726/19/10/10500410.1088/0964-1726/19/10/105004 ↗
30. 10.1088/0964-1726/18/9/09500610.1088/0964-1726/18/9/095006 ↗
31. 10.1016/j.compstruct.2014.11.03110.1016/j.compstruct.2014.11.031 ↗
32. 10.1364/AO.38.00016810.1364/AO.38.000168 ↗