Steering Mirror System with Closed-Loop Feedback for Free-Space Optical Communication Terminals
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Published:2024-04-23
Issue:5
Volume:11
Page:330
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ISSN:2226-4310
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Container-title:Aerospace
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language:en
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Short-container-title:Aerospace
Author:
Graham Chris1ORCID, Bramall David1, Younus Othman2ORCID, Riaz Amna2, Binns Richard2, Scullion Eamon2ORCID, Wicks Robert T.2ORCID, Bourgenot Cyril1ORCID
Affiliation:
1. Centre for Advanced Instrumentation, Durham University, NETPark Research Institute, Joseph Swan Road, Sedgefield TS21 3FB, UK 2. Department of Mathematics, Physics and Electrical Engineering, Northumbria University, Newcastle upon Tyne NE1 8ST, UK
Abstract
Precision beam pointing plays a critical role in free-space optical communications terminals in uplink, downlink and inter-satellite link scenarios. Among the various methods of beam steering, the use of fast steering mirrors (FSM) is widely adopted, with many commercial solutions employing diverse technologies, particularly focusing on small, high-bandwidth mirrors. This paper introduces a method using lightweight, commercial off-the-shelf components to construct a custom closed-loop steering mirror platform, suitable for mirror apertures exceeding 100 mm. The approach involves integrating optical encoders into two off-the-shelf open-loop actuators. These encoders read the signal reflected on purposefully diamond-machined knurled screw knobs, providing maximum contrast between light and dark lines. The resulting steering mirror has the potential to complement or replace FSM in applications requiring a larger stroke, at the expense of motion speed. In the presented setup, the mirror tilt resolution achieved based on the encoder closed-loop signal feedback is 45 μrad, with a mean slew rate of 1.5 mrad/s. Importantly, the steering assembly is self-locking, requiring no power to maintain a steady pointing angle. Using the mirror to actively correct for a constantly moving incoming beam, a 5-fold increase in concentration of the beam spot on the center of the detector was obtained compared to a fixed position mirror, demonstrating the mirrors ability to correct for satellite platform jitter and drift.
Reference19 articles.
1. Broadband LEO Satellite Communications: Architectures and Key Technologies;Su;IEEE Wirel. Commun.,2019 2. A Survey on Acquisition, Tracking, and Pointing Mechanisms for Mobile Free-Space Optical Communications;Kaymak;IEEE Commun. Surv. Tutor.,2018 3. Fields, R., Kozlowski, D., Yura, H., Wong, R., Wicker, J., Lunde, C., Gregory, M., Wandernoth, B., and Heine, F. (2011, January 11–13). 5.625 Gbps bidirectional laser communications measurements between the NFIRE satellite and an Optical Ground Station. Proceedings of the 2011 International Conference on Space Optical Systems and Applications (ICSOS’11), Santa Monica, CA, USA. 4. Kolev, D., Takenaka, H., Munemasa, Y., Akioka, M., Iwakiri, N., Koyama, Y., Kunimori, H., Toyoshima, M., Artaud, G., and Issler, J.L. (2015, January 26–28). Overview of international experiment campaign with small optical transponder (SOTA). Proceedings of the 2015 IEEE International Conference on Space Optical Systems and Applications (ICSOS), New Orleans, LA, USA. 5. Schmidt, C., Rödiger, B., Rosano, J., Papadopoulos, C., Hahn, M.T., Moll, F., and Fuchs, C. (2022, January 29–31). DLR’s Optical Communication Terminals for CubeSats. Proceedings of the 2022 IEEE International Conference on Space Optical Systems and Applications (ICSOS), Virtual.
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