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Optical Modeling Activities for NASA's James Webb Space Telescope (JWST): III. Wavefront Aberrations due to Alignment and Figure Compensation

机译:美国宇航局的James Webb太空望远镜(JWST)的光学建模活动:III。波前像差由于对齐和数字补偿

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This paper is part three of a series describing the ongoing optical modeling activities for the James Webb Space Telescope (JWST). The first two papers discussed modeling JWST on-orbit performance using wavefront sensitivities to predict line of sight motion induced blur, and stability during thermal transients [1-2]. The work here investigates the aberrations resulting from alignment and figure compensation of the controllable degrees of freedom (i.e. the primary and secondary mirrors), which may be encountered during ground alignment and on-orbit commissioning of the observatory. The optical design of the telescope is a three-mirror anastigmat, with an active fold mirror at the exit pupil for fine guiding. The primary mirror is over 6.5 meters in diameter, and is composed of 18 hexagonal segments that can individually positioned on hexapods, as well as compensated for radius of curvature. This architecture effectively gives both alignment and figure control of the primary mirror. The secondary mirror can be moved in rigid body only, and the tertiary mirror is fixed. Simulations are performed of various combinations of alignment and figure errors corrected by the primary and secondary mirrors. Single field point knowledge is assumed in the corrections, and aberrations over the field are reported for the varying cases.
机译:本文是一个系列的第三部分,描述了詹姆斯韦布斯太空望远镜(JWST)的正在进行的光学建模活动。前两篇论文使用波前敏感性讨论了JWST轨道性能,以预测视觉运动引起的模糊线,以及热瞬变期间的稳定性[1-2]。这里的作品研究了由对准和图形补偿产生的像差,这些像差是可控制的自由度(即初级和次镜),这在地面对准和天文台的轨道调试期间可能会遇到。望远镜的光学设计是一个三镜子anaStigmat,在出口瞳孔处有一个有源折叠镜,用于精细指导。主镜直径超过6.5米,由18个六边形段组成,可以单独定位在六边形段上,以及补偿曲率半径。这种架构有效地给出了主镜的对齐和图形控制。二次镜子可以仅在刚体中移动,并且第三镜是固定的。对由主镜和次级镜校正的各种对准组合和图形误差进行仿真。在校正中假设单个场点知识,并且报告了该字段上的像差对于变化的情况。

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