首页> 外文期刊>South African Journal of Geology: Being the Transaction of the Geological Society of South African: Syndie die Verhandelinge van die Geologiese Vereniging van Suid-Afrika >A proposed mathematical model of thermal variations on the HartRAO Lunar Laser Ranging telescope for enhanced test of Earth-Moon system dynamics
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A proposed mathematical model of thermal variations on the HartRAO Lunar Laser Ranging telescope for enhanced test of Earth-Moon system dynamics

机译:Hartrao Lunar激光测距望远镜热变化的提出数学模型,用于增强地球系统动态的试验

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摘要

A new geodetic observatory at Matjiesfontein will house a 1-metre aperture Lunar Laser Ranging (LLR) optical telescope to acquire millimetre Earth-Moon distance measurements. Large optical telescopes utilised for laser ranging observations of Earth-Moon distance, with sub-centimetre level accuracy can suffer from structural deformations induced by thermal variations, wind loadings and/ or gravitational forces. These variables need to be measured to enable correction of the resulting pointing errors. This paper presents the proposed locations of temperature sensors on the composite structure of the Hartebeesthoek Radio Astronomy Observatory (HartRAO) LLR 1-metre optical telescope. Furthermore, we describe a mathematical model for (i) obtaining thermal measurements from a network of temperature sensors, (ii) interpolating the temperatures across the telescope composite structure, and (iii) predicting thermally-induced structural deformations. Currently, the available thermal simulation results of the LLR telescope tube assembly indicate isotherms with gradients of about 1°C followed by thermal deformations that vary between 2.9 μm and 40.7 μm along the optical tube axes. The physical implementation of the above mathematical model is part of the next phase of this research work coupled with experiments to derive thermally-induced pointing errors. The errors will be incorporated into the steering control software to compensate for thermally-induced misalignment of the telescope axes.
机译:MatjiesFontein的新型大地测量学天文台将在1米的孔径月球激光测距(LLR)光学望远镜上,以获得毫米的地球距离测量。用于激光测距的大型光学望远镜的地球距离,具有亚厘米级精度可以遭受由热变化,风机和/或重力诱导的结构变形。需要测量这些变量以实现所产生的指向误差的校正。本文介绍了Hartebeesthoek射频天文学天文台(Hartrao)LLR 1米光学望远镜的复合结构上的温度传感器的建议位置。此外,我们描述了(i)从温度传感器网络获得热测量的数学模型,(ii)在望远镜复合结构上插入温度,(iii)预测热诱导的结构变形。目前,LLR望远镜管组件的可用热仿真结果表明等温线的梯度约为1°C,然后沿光学管轴在2.9μm和40.7μm之间变化的热变形。上述数学模型的物理实施是该研究的下一阶段的一部分,其与实验相结合,以获得热诱导的指向误差。误差将结合到转向控制软件中以补偿望远镜轴的热诱导的未对准。

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