Architecture and performance analysis of an optical metrology terminal for satellite-to-satellite laser ranging

被引:8
|
作者
Mandel, Oliver [1 ,2 ]
Sell, Alexander [2 ]
Chwalla, Michael [2 ]
Schuldt, Thilo [1 ,3 ]
Krauser, Jasper [2 ]
Weise, Dennis [2 ]
Braxmaier, Claus [1 ,3 ]
机构
[1] Univ Bremen, Ctr Appl Space Technol & Micrograv ZARM, D-28359 Bremen, Germany
[2] Airbus Def & Space GmbH, D-88039 Friedrichshafen, Germany
[3] German Aerosp Ctr DLR, D-28359 Bremen, Germany
关键词
Tracking; (position);
D O I
10.1364/AO.378658
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
Interferometric laser ranging is an enabling technology for high-precision satellite-to-satellite tracking within the context of Earth observation, gravitational wave detection, or formation flying. In orbit, the measurement system is affected by environmental influences, particularly satellite attitude jitter and temperature fluctuations, imposing an instrument design with a high level of thermal stability and insensitivity to rotations around the spacecraft center of mass. The new design concept presented here combines different approaches for dynamic heterodyne laser ranging and features the inherent beam-tracking capabilities of a retroreflector in a mono-axial configuration. It allows for a continuously adjustable distance between the optical bench and the location of its fiducial point, facilitating future inter-satellite tracking with nanometer accuracy, e.g., the next-generation gravity mission. (C) 2020 Optical Society of America.
引用
收藏
页码:653 / 661
页数:9
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