An adaptive calibration and beamforming technique for a GEO satellite data relay. (23rd May 2017)

• Record Type: Journal Article
• Authors: Winterstein, Andreas; Greda, Lukasz A.
• Is Part Of: International journal of satellite communications and networking. Volume 36:Number 2(2018)
• Page Start: 207
• Page End: 219
• Publication Date: 2017-05-23
• Subjects: adaptive signal processing -- beamforming -- calibration -- least mean squares methods -- reflector antennas; Artificial satellites in telecommunication -- Periodicals; Digital communications -- Periodicals; 621.3825
• DOI: 10.1002/sat.1213
• Languages: English
• ISSNs: 1542-0973

Abstract

Summary: High throughput data links from low Earth orbit satellites through a geostationary orbit satellite data relay have been proposed to increase the available contact times to ground stations. Accurate antenna beam pointing and tracking of moving targets are key requirements for the relay satellite. In this work, we propose an adaptive calibration and beamforming methodology on the basis of least mean squares, which is suitable for a geostationary orbit data relay. The target system consists of the combination of a high gain reflector fed by a digitally steerable patch antenna array. The proposed method is first presented by numerical cosimulation of the antenna and the calibration algorithm. The results are then validated in an outdoor experimental setup with all digital signal processing implemented in a field‐programmable gate array. We demonstrate the tracking ability and pointing performance of the digitally enhanced reflector antenna with gain fluctuations smaller than 3 dB over a field of view of at least 2, 5°. The demonstrated performance shows that the digitally enhanced reflector antenna is a suitable candidate for long‐distance space communications. Abstract : A digitally enhanced multibeam antenna using the array‐fed reflector principle is proposed. It shall be used on a geostationary orbit satellite acting as a communication relay for several low Earth orbit satellites.We present numerical cosimulation results and an experimental validation of the system concept.