Automated monitoring of flatness of solar array wings

Space engineering and technology Pub Date : 2022-03-31 DOI:10.33950/spacetech-2308-7625-2022-1-70-79

Vladimir I. Marinin, Sergey M. Zhurikhin, D. Kireev, Dmitry Andreev, N. Andreeva, N. I. Kopyl, Aleksandr N. Senkovskiy, Sergey F. Ilyushenkov, S. N. Churkin

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Abstract

This article discusses capabilities of a new special-purpose software-measuring system for monitoring flatness of solar array (SA) wings. The performance data and specifics of work are presented. The specifics of measurement of SA wings flatness are described. The allowable deviations from flatness of SA wings of the science power module (SPM) as part of the International Space station are given. The composition of the measuring complex is developed. The visual approach of making plans for testing methods and measurement techniques based on visual components is considered in detail. The elements from which the measurement plans are built are considered. Sample plans for verification procedures, methods of measuring flatness of the front and back wing surfaces are provided. Basic requirements for processing of measurement results which are stored for compatibility with the old manual approach of measurements are specified. Basic measurement processing algorithms for calculation of general and local wing out-of-flatness are provided. Key words: SA wing, solar array wing, meter, component model, overview, general out-of-flatness, local out-of-flatness.

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太阳能电池板翼面平整度的自动监测

本文讨论了一种用于太阳能电池阵列(SA)翼面平整度监测的专用软件测量系统的性能。给出了性能数据和工作细节。介绍了气动机翼平整度测量的具体方法。给出了作为国际空间站一部分的科学动力模块(SPM)的SA翼的允许平面偏差。研究了测量配合物的组成。详细讨论了基于可视化组件的测试方法和测量技术计划的可视化方法。要考虑构建度量计划的元素。提供了验证程序和测量前、后翼表面平整度的方法的样品计划。为与旧的手动测量方法兼容而存储的测量结果处理的基本要求被规定。给出了计算总翼差和局部翼差的基本测量处理算法。关键词:SA翼，太阳能阵列翼，仪表，部件模型，概述，整体失平度，局部失平度。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Space engineering and technology

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