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Two-laser heterodyne metrology for a separated spacecraft interferometer

机译:分离航天器干涉仪的两激光外差测量

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Abstract: The proposed New Millennium Interferometer consists of three spacecraft separated by up to several kilometers. A heterodyne laser metrology system is proposed to measure the relative distances between the spacecraft. Because diffraction losses for a round-trip measurement are prohibitively large, a two-laser metrology system has been suggested in which each spacecraft has both a laser and a receiver. The system has been successfully demonstrated with a one meter baseline and verified by a conventional single- laser system in a laboratory experiment. The precision was limited by thermal effects in the room environment for time scales greater than one minute. The single-laser system obtained a precision of 3 nm for integration times up to 0.5 seconds. The two-laser system obtained a precision of 20 and was limited by self-interference and electronics noise. The resolution of the two-laser metrology system was $lambda@30.!9
机译:摘要:拟议中的新千年干涉仪由三个相隔数公里的航天器组成。提出了一种外差激光计量系统来测量航天器之间的相对距离。由于往返测量的衍射损耗过大,因此提出了一种两激光测量系统,其中每个航天器都同时具有激光和接收器。该系统已成功以一米的基线进行了演示,并在实验室实验中通过传统的单激光系统进行了验证。对于超过一分钟的时间标度,精度受到房间环境中的热效应的限制。单激光系统的积分时间高达0.5秒,精度为3 nm。两激光系统的精度为20,并且受到自干扰和电子噪声的限制。两激光测量系统的分辨率为$lambda@30.!9

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