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Global alignment optimization strategies, procedures, and tools for the James Webb Space Telescope (JWST) Integrated Science Instrument Module (ISIM)

机译:詹姆斯·韦伯太空望远镜(JWST)集成科学仪器模块(ISIM)的全局对准优化策略,过程和工具

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During cryogenic vacuum testing of the James Webb Space Telescope (JWST) Integrated Science Instrument Module(ISIM), the global alignment of the ISIM with respect to the designed interface of the JWST optical telescope element(OTE) will be measured through a series of optical characterization tests. These tests will determine the locations andorientations of the JWST science instrument projected focal surfaces and entrance pupils with respect to theircorresponding OTE optical interfaces. Thermal, finite element and optical modeling will then be used to predict the on-orbitoptical performance of the observatory. If any optical performance non-compliances are identified, the ISIM willbe adjusted to improve its performance. If this becomes necessary, ISIM has a variety of adjustments that can be made.The lengths of the six kinematic mount struts that attach the ISIM to the OTE can be modified and five scienceinstrument focus positions and two pupil positions can be individually adjusted as well. In order to understand how tomanipulate the ISIM’s degrees of freedom properly and to prepare for the ISIM flight model testing, we have completeda series of optical-mechanical analyses to develop and identify the best approaches for bringing a non-compliant ISIMElement back into compliance. During this work several unknown misalignment scenarios were produced and thesimulated optical performance metrics were input into various mathematical modeling and optimization tools todetermine how the ISIM degrees of freedom should be adjusted to provide the best overall optical performance.© (2012) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
机译:在詹姆斯·韦伯太空望远镜(JWST)集成科学仪器模块(ISIM)的低温真空测试期间,将通过一系列光学手段来测量ISIM相对于JWST光学望远镜元件(OTE)的设计接口的全局对准。表征测试。这些测试将确定JWST科学仪器投射的焦面和入射光瞳相对于其对应的OTE光学界面的位置和方向。然后,将使用热,有限元和光学建模来预测天文台的在轨光学性能。如果发现任何光学性能不符合项,将对ISIM进行调整以提高其性能。如果有必要,可以对ISIM进行各种调整。可以将将ISIM固定在OTE上的六个运动安装支杆的长度进行修改,还可以分别调整五个科学仪器的聚焦位置和两个瞳孔位置。为了了解如何正确操纵ISIM的自由度并为ISIM飞行模型测试做准备,我们完成了一系列的光学机械分析,以开发和确定使不符合标准的ISIMElement恢复合规的最佳方法。在这项工作期间,产生了几种未知的未对准情况,并将模拟的光学性能指标输入到各种数学建模和优化工具中,以确定应如何调整ISIM自由度以提供最佳的总体光学性能。©(2012)COPYRIGHT Society of Photo-光学仪器工程师(SPIE)。摘要的下载仅允许个人使用。

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