Measuring Antenna Elevation Mechanism Pointing Errors with Multiencoder Information Sources

IF 1.6 4区 物理与天体物理 Q3 ASTRONOMY & ASTROPHYSICS Advances in Astronomy Pub Date : 2023-04-13 DOI:10.1155/2023/3527106
Duoxiang Xu, Qian Xu, Na Wang, Fei Xue
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Abstract

There are many factors that cause pointing errors in radio telescopes. As one of the motion positioning mechanisms of the radio telescope, the error caused by the elevation mechanism cannot be ignored. The source of error in the elevation mechanism comes mainly from the key transmission components and the support structure. Accurate measurement of the errors caused by them is the key to analyzing their law of change. Aiming at the main error factors in the antenna elevation mechanism, this study builds a scaled-down experimental platform for the elevation mechanism and proposes an error measurement method based on multiencoder information sources. The method compares the error law of change of the antenna elevation mechanism under different driving modes, different centerline deviations of the bearings, and different backlashes and designs error measurement experiments for the abovementioned operating conditions. The results show that the error measurement method based on multiencoder information sources can accurately measure the error of the antenna elevation mechanism under different driving modes. The method can also accurately reflect the law of change in transmission error when the backlash of the elevation mechanism and the centerline deviation of the bearings increase. The final experimental measurement shows that the driving mode of the dual-motor can eliminate about 70% of the mechanism error caused by the backlash. The average value of the error increases by a factor of 1.9 when the backlash increases from 0.1 mm to 1.26 mm. The average value of the error increases by a factor of 5 when the centerline deviation of the bearings increases from 0 to 1.5 mm. This has a good reference value to correct for the pointing error of a radio telescope.
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利用多编码器信息源测量天线仰角机构指向误差
导致射电望远镜指向误差的因素有很多。仰角机构作为射电望远镜的运动定位机构之一,其产生的误差不容忽视。高程机构的误差来源主要来自关键传动部件和支撑结构。准确测量其误差是分析其变化规律的关键。针对天线仰角机构的主要误差因素,构建了按比例缩小的仰角机构实验平台,提出了一种基于多编码器信息源的误差测量方法。该方法比较了天线俯仰机构在不同驱动方式、轴承不同中心线偏差、不同间隙下的误差变化规律,并针对上述工况设计了误差测量实验。结果表明,基于多编码器信息源的误差测量方法能够准确测量出不同驱动模式下天线俯仰机构的误差。该方法还可以准确地反映当仰角机构的间隙和轴承的中心线偏差增加时传动误差的变化规律。最后的实验测量表明,双电机驱动方式可消除由间隙引起的机构误差约70%。当间隙从0.1 mm增加到1.26 mm时,误差的平均值增加了1.9倍。当轴承的中心线偏差从0增加到1.5 mm时,误差的平均值增加了5倍。这对修正射电望远镜的指向误差有很好的参考价值。
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来源期刊
Advances in Astronomy
Advances in Astronomy ASTRONOMY & ASTROPHYSICS-
CiteScore
2.70
自引率
7.10%
发文量
10
审稿时长
22 weeks
期刊介绍: Advances in Astronomy publishes articles in all areas of astronomy, astrophysics, and cosmology. The journal accepts both observational and theoretical investigations into celestial objects and the wider universe, as well as the reports of new methods and instrumentation for their study.
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