Inter-satellite optical communication link

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Abstract

A two-level system of data transmission in the optical range is considered between a low-orbit spacecraft located in a sun-synchronous orbit and a repeater satellite located in a geostationary orbit. This topic is rather relevant due to the fact that the rapid development of remote sensing satellites resulted in the increase of the amount of transmitted information, which in consequence introduced new requirements for communication systems. The increase of data transmission rate and severization of requirements for communication systems contributed to the development of one of the most promising areas of space communications, based on the information transmission via a laser channel, due to a high energy concentration and a much higher carrier frequency. The prospects for the application of optical communication systems are designated by lower power consumption, dimensional specifications and the mass of the transceiver equipment of the optical range (compared to radiofrequency range systems).

The article describes the solution of application of optical communication link between a low-orbit spacecraft and a repeater satellite. The main factors that contribute to the attenuation in the process of signal propagation along the route are presented and analyzed. A model of a communication channel between a low-orbit spacecraft and a repeater satellite is provided for a visual image. Two different approaches of mutual guidance and tracking of laser terminals are described for using beacons and without ones. EDRS foreign system is considered as an analogue. The estimation of the main parameters of the communication link is given.

The communication system considered in the article will allow for greater carrier capacity of the data transmission in the optical range between the low-orbit spacecraft and repeater satellite. The application of this system will allow solving problems, including in the interests of any departments and structures of the Ministry of Defense of the Russian Federation, for which the rate of obtaining information is one of the basic requirements for a satellite communication system. The tasks of precise targeting of receiving and transmitting devices arising as a result of narrow beam patterns can be solved with current technical means.

About the authors

Aleksandr V. Aleksandrov

Kirensky Institute of Physics – Federal Research Center “Krasnoyarsk Scientific Center” Siberian Branch of the Rus-sian Academy of Sciences

Email: alexa820@mail.ru

Postgraduate student

Russian Federation, 50, bldg. 38, Akademgorodok St., Krasnoyarsk, 660036

Aleksandr V. Vasilenko

JSC “Academician M. F. Reshetnev “Information Satellite Systems”

Email: a.v.vasilenko@mail.ru

Leading Engineer

Russian Federation, 52, Lenin St., Zheleznogorsk, Krasnoyarsk region, 662972

Dmitry O. Korolev

Siberian Federal University

Author for correspondence.
Email: korolyov.93@gmail.com

Postgraduate student

Russian Federation, 79, Svobodny Av., Krasnoyarsk, 660041

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Copyright (c) 2019 Aleksandrov A.V., Vasilenko A.V., Korolev D.O.

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