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SOFIA Secondary Mirror Mechanism Heavy Maintenance and Improvements

机译:索非亚二级镜机制重维护和改进

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The Stratospheric Observatory For Infrared Astronomy (SOFIA) reached its full operational capability in 2014 and completed hundreds of observation flights. Since its installation in 2002, the Secondary Mirror Mechanism was subject to thousands of operating hours equivalent to millions of load cycles. During the aircraft heavy maintenance in fall 2014, a four month time window enabled the removal of the mechanism from the telescope structure for service and improvements. Next to visual corrosion- and crack-inspection of the flexures, critical electronic components (in particular the set of three eddy current position sensors that determine the mirror tilt) were replaced. Moreover, a detailed temperature dependent position calibration of the system was performed in a cold chamber to improve the pointing accuracy. Until then, a simple temperature independent linear gain was used to translate the sensor output voltage into a position. For accurate positioning across the whole temperature range, a temperature dependent correction function had to be developed. This calibration would have cost hours of observing time when performed in flight which made it an essential goal for completion during the maintenance period. An autocollimator was used as optical reference camera to measure the tip-tilt position of the secondary mirror in the cold chamber. Using this calibration setup, a pattern of many mirror positions in the tip-tilt domain was approached at several temperature points to provide a high resolution data set for the new multidimensional calibration function. Follow-up in-flight verification measurements confirmed a large improvement in pointing accuracy as soon as the temperature measurements were included into the position correction. Improvements of up to a factor of 10 were especially noticed in the lower temperature range. This contribution provides an insight into the work performed during the SOFIA - Secondary Mirror Mechanism maintenance with the focus on the temperature dependent position calibration.
机译:红外天文学(索非亚)的平流层天文​​台于2014年达到了完全的运营能力,并完成了数百种观察航班。自2002年安装以来,二次镜子机制受数千万次负载循环的运行。在2014年秋季的飞机重型维护期间,一个四个月的时间窗口使得从望远镜结构中移除机构以进行服务和改进。在弯曲的视觉腐蚀和裂缝检查旁边,临界电子元件(特别是确定镜子倾斜的三个涡流位置传感器)被替换。此外,在冷室中进行系统的详细温度依赖位置校准,以提高指向精度。在此之前,使用简单的温度独立线性增益将传感器输出电压转换为位置。为了精确定位整个温度范围,必须开发温度依赖性校正功能。在飞行中执行时,此校准将具有成本时间的观察时间,这使其成为维护期间完成的必要目标。用作光学参考摄像机的自电管器以测量冷室中的次镜的尖端倾斜位置。使用该校准设置,在若干温度点处接近尖端倾斜域中许多镜像位置的图案,以提供新的多维校准功能的高分辨率数据集。一旦将温度测量输出到位置校正中,就会在飞行中验证测量结果证实了指向精度的大大提高。在较低温度范围内特别注意到高达10倍的改善。此贡献提供了对索非亚 - 二次镜像机构维护期间执行的工作的洞察,并专注于温度相关的位置校准。

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