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Journal Article

Design and qualification of a recessed satellite cornercube retroreflector for ground-based attitude verification via satellite laser ranging

Authors

Bartels,  Nils
External Organizations;

Allenspacher,  Paul
External Organizations;

/persons/resource/sbauer

Bauer,  Sven
1.2 Global Geomonitoring and Gravity Field, 1.0 Geodesy, Departments, GFZ Publication Database, Deutsches GeoForschungsZentrum;

Rödiger,  Benjamin
External Organizations;

Sproll,  Fabian
External Organizations;

Riede,  Wolfgang
External Organizations;

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4476889.pdf
(Publisher version), 6MB

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Citation

Bartels, N., Allenspacher, P., Bauer, S., Rödiger, B., Sproll, F., Riede, W. (2019): Design and qualification of a recessed satellite cornercube retroreflector for ground-based attitude verification via satellite laser ranging. - CEAS Space Journal, 11, 4, 391-403.
https://doi.org/10.1007/s12567-019-00255-x


Cite as: https://gfzpublic.gfz-potsdam.de/pubman/item/item_4476889
Abstract
The design and qualification of a retroreflector specifically designed for a CubeSat (CubeL) is described. The CubeSat will be launched to space in 2019 and demonstrate the latest generation of the optical space infrared downlink system developed by the German Aerospace Center together with the industrial partner Tesat-Spacecom. The retroreflector is optimized to allow for a coarse verification of the satellites attitude control system. By analyzing the returning photon count during satellite laser ranging (SLR) when the satellite is operated in station pointing mode attitude information is obtained. To achieve this goal, the entrance face of the retroreflector is recessed by a circular tube-shaped aperture. Due to this recession, the signal reflected from the retroreflector falls off rapidly when the retroreflector is tilted away from the SLR station. From measurements of the retroreflectors far-field diffraction pattern and calculations, we believe that it should be possible to determine the orientation accuracy of the satellite to within ± 2°. The proposed method is an effective and cheap way for coarse attitude control, e.g., for satellites of mega-constellations with any existing satellite laser ranging ground station.