TY - JOUR
T1 - Accuracy of satellite orbit prediction and optical design of optical ground station beacons for satellite-to-ground optical communication
AU - Takenaka, H.
AU - Kunimori, H.
AU - Fujita, S.
AU - Kuwahara, T.
AU - Kubooka, T.
AU - Fuse, T.
AU - Toyoshima, M.
N1 - Funding Information:
This research and development work was supported by the MIC/SCOPE # 191502001.
Publisher Copyright:
© 2021 ESA and CNES
PY - 2021
Y1 - 2021
N2 - In recent years, spatial optical communication has been attracting attention as a large-capacity communication method that connects satellites and the ground. Radiofrequency communications are used as a method for transmitting data acquired by satellites to the ground. However, the radio frequencies used make it difficult to improve the communication speed, owing to interference problems and the carrier frequency. Space optical communication is expected to be a solution to this issue. A beacon method is often used to emit light from an optical ground station toward a satellite for initial acquisition. It is desirable that the divergence angle of the irradiating beacon covers the range of satellite orbit prediction. Therefore, it is important to know the orbit prediction accuracy of a satellite. In the experiment, satellite flare was observed from a ground station and verified by comparing the telescope tracking data with the GPS data and NORAD-TLE information mounted on the satellite.
AB - In recent years, spatial optical communication has been attracting attention as a large-capacity communication method that connects satellites and the ground. Radiofrequency communications are used as a method for transmitting data acquired by satellites to the ground. However, the radio frequencies used make it difficult to improve the communication speed, owing to interference problems and the carrier frequency. Space optical communication is expected to be a solution to this issue. A beacon method is often used to emit light from an optical ground station toward a satellite for initial acquisition. It is desirable that the divergence angle of the irradiating beacon covers the range of satellite orbit prediction. Therefore, it is important to know the orbit prediction accuracy of a satellite. In the experiment, satellite flare was observed from a ground station and verified by comparing the telescope tracking data with the GPS data and NORAD-TLE information mounted on the satellite.
KW - FSO
KW - Satellite orbit prediction
KW - Two Line Element
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U2 - 10.1117/12.2599372
DO - 10.1117/12.2599372
M3 - Conference article
AN - SCOPUS:85116058634
SN - 0277-786X
VL - 11852
JO - Proceedings of SPIE - The International Society for Optical Engineering
JF - Proceedings of SPIE - The International Society for Optical Engineering
M1 - 118522C
T2 - 2020 International Conference on Space Optics, ICSO 2020
Y2 - 30 March 2021 through 2 April 2021
ER -