Research output: Contribution to journal › Article › peer-review
First Flight-Testing of LoRa Modulation in Satellite Radio Communications in Low-Earth Orbit. / Zadorozhny, Alexander M.; Doroshkin, Alexander A.; Gorev, Vasily N. et al.
In: IEEE Access, Vol. 10, 2022, p. 100006-100023.Research output: Contribution to journal › Article › peer-review
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TY - JOUR
T1 - First Flight-Testing of LoRa Modulation in Satellite Radio Communications in Low-Earth Orbit
AU - Zadorozhny, Alexander M.
AU - Doroshkin, Alexander A.
AU - Gorev, Vasily N.
AU - Melkov, Alexander V.
AU - Mitrokhin, Anton A.
AU - Prokopyev, Vitaliy Yu
AU - Prokopyev, Yuri M.
N1 - Publisher Copyright: © 2013 IEEE.
PY - 2022
Y1 - 2022
N2 - At present, the use of LoRa modulation in satellite radio communications and the construction of a CubeSat constellation for the satellite Internet of Things based on LoRa technology has already begun. However, the limits of applicability of LoRa modulation in low-Earth orbits have not yet been established. This paper presents the results of the first flight tests of LoRa modulation for robustness against the Doppler effect in the satellite-to-Earth radio channel, carried out using a NORBY CubeSat operating at 560 km. Flight tests confirmed the very high immunity of LoRa modulation to the Doppler effect for modes with spreading factor SF ≤ 11 and spread spectrum modulation bandwidth BW > 31.25 kHz. LoRa modulation in these modes can be used in satellite communication without any limitations caused by the Doppler effect. For BW = 31.25 kHz, the LoRa radio channel is affected by the static Doppler effect. Communication with the satellite is possible in this case only at high elevation angles. For SF = 12, the dynamic Doppler effect becomes significant, and communication is possible only at low satellite elevation angles, which leads to the formation of a 'hole' in the center of the coverage area directly below the satellite. In both cases, the duration of the communication session is significantly reduced because of the Doppler effect. In the case of SF = 11 and 12 at BW = 31.25 kHz, both static and dynamic Doppler effect catastrophically affect the LoRa radio channel, so that communication with the satellite becomes impossible.
AB - At present, the use of LoRa modulation in satellite radio communications and the construction of a CubeSat constellation for the satellite Internet of Things based on LoRa technology has already begun. However, the limits of applicability of LoRa modulation in low-Earth orbits have not yet been established. This paper presents the results of the first flight tests of LoRa modulation for robustness against the Doppler effect in the satellite-to-Earth radio channel, carried out using a NORBY CubeSat operating at 560 km. Flight tests confirmed the very high immunity of LoRa modulation to the Doppler effect for modes with spreading factor SF ≤ 11 and spread spectrum modulation bandwidth BW > 31.25 kHz. LoRa modulation in these modes can be used in satellite communication without any limitations caused by the Doppler effect. For BW = 31.25 kHz, the LoRa radio channel is affected by the static Doppler effect. Communication with the satellite is possible in this case only at high elevation angles. For SF = 12, the dynamic Doppler effect becomes significant, and communication is possible only at low satellite elevation angles, which leads to the formation of a 'hole' in the center of the coverage area directly below the satellite. In both cases, the duration of the communication session is significantly reduced because of the Doppler effect. In the case of SF = 11 and 12 at BW = 31.25 kHz, both static and dynamic Doppler effect catastrophically affect the LoRa radio channel, so that communication with the satellite becomes impossible.
KW - CubeSat
KW - Doppler effect
KW - LoRa modulation
KW - low-Earth orbit
KW - on-orbit flight test
KW - satellite IoT
KW - satellite radio communication
KW - the Internet of Things
UR - http://www.scopus.com/inward/record.url?scp=85139450467&partnerID=8YFLogxK
U2 - 10.1109/ACCESS.2022.3207762
DO - 10.1109/ACCESS.2022.3207762
M3 - Article
AN - SCOPUS:85139450467
VL - 10
SP - 100006
EP - 100023
JO - IEEE Access
JF - IEEE Access
SN - 2169-3536
ER -
ID: 38153102