SPICA SAFARI仪器傅里叶变换光谱仪新型低温刚度补偿无反应扫描机构设计

A. Cournoyer, Éric Carbonneau, P. Gilbert, L. Bibeau, Simon Houle, Hugo Bourque, I. Silversides, F. Grandmont, D. Naylor, B. Gom, Sudhakar Gunuganti, D. Loon, W. Jellema
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引用次数: 3

摘要

SpicA远红外仪器(SAFARI)的高光谱分辨率模式是通过在仪器的信号通路中插入一个基于马丁-普普莱特干涉仪的傅立叶变换光谱仪(FTS)实现的。低温机制(FTSM)使两个背靠背的屋顶镜子共享一个共同的顶点进行线性扫描。ABB公司与加拿大航天局签订合同,为TRL-5演示开发和测试4 K的FTSM工程演示单元(EDU)。SAFARI FTSM性能的主要驱动因素是严格的机电要求(车顶反射镜的位置稳定性<10 nm RMS, <34 mm线性行程),在特定的微振动环境(外部30 μg/√Hz)下严格的热平衡(散热<1.5 mW),所有这些都是在低温(4 K)下进行的。在本文中,我们描述了一种新型的低温FTSM设计,采用无反应和长行程基于挠度的4杆连杆与刚度补偿。该1-DOF机构通过弯曲轴被动控制车顶反射镜的导向,而轴向扫描由定制的移动磁体执行器(MMA)驱动和控制。FTSM的静态和动态平衡确保将低振动水平传递到/从FTSM底板传递,并且机构刚度的补偿将MMA所需的力和驱动电流降低了小于10倍。这两个特性导致MMA的功耗/耗散<1.5 mW。对FTSM EDU动态模型的工程分析结果进行了讨论,以评估该设计是否符合具有挑战性的低温SAFARI FTSM性能要求。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design of a novel cryogenic stiffness-compensated reactionless scan mechanism for the Fourier transform spectrometer of SPICA SAFARI instrument
The high spectral resolution mode of the SpicA FAR-infrared Instrument (SAFARI) is enabled by inserting a Fourier Transform Spectrometer (FTS), based on a Martin-Puplett interferometer, into the signal path of the instrument. The cryogenic mechanism (FTSM) enables linear scans of two back-to-back rooftop mirrors sharing a common apex. ABB Inc. is under contract with the Canadian Space Agency to develop and test at 4 K an FTSM Engineering Demonstration Unit (EDU) for TRL-5 demonstration. The main SAFARI FTSM performance drivers are the stringent mechatronic demands (position stability of roof-top mirrors <10 nm RMS, <34 mm linear stroke), severely constrained by a tight thermal budget (heat dissipation <1.5 mW) under a specific micro-vibrations environment (30 μg/√Hz external), all at cryogenic temperatures (4 K). In this paper, we describe a novel cryogenic FTSM design using a reactionless and longstroke flexure-based 4-bar linkage with stiffness compensation. This 1-DOF mechanism passively controls the guiding of the roof-top mirrors with flex pivots while the axial scanning is actuated and controlled with a custom moving magnet actuator (MMA). Static and dynamic balancing of the FTSM ensures that low vibration levels are transferred to/from the FTSM baseplate, and compensation of the mechanism stiffness reduces the force and drive current required from the MMA by a factor <10. Both features lead to MMA power consumption/dissipation <1.5 mW. Results from an engineering analysis of a dynamic model developed for the FTSM EDU are discussed to assess the compliance of this design to the challenging cryogenic SAFARI FTSM performance requirements.
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