Тип публикации: доклад, тезисы доклада, статья из сборника материалов конференций
Конференция: International Siberian Conference on Control and Communications (SIBCON); Tomsk State Univ Control Syst & Radioelectron, Tomsk, RUSSIA; Tomsk State Univ Control Syst & Radioelectron, Tomsk, RUSSIA
Год издания: 2019
Ключевые слова: range measurement, spacecraft, geostationary orbit, measurement accuracy, satellite earth station, timing, satellite communications, tracking telemetry and command subsystem, pseudo-random sequence, delay time, difference in phase, multi-frequency method
Аннотация: As a result of the gravitational attraction of the Sun/Moon/Earth, the pressure of solar radiation and other factors, the spacecraft located in the geostationary orbit deviates from the real orbit. The position of the spacecraft is regulated by a short pu
Журнал: 2019 INTERNATIONAL SIBERIAN CONFERENCE ON CONTROL AND COMMUNICATIONS (SIBCON)
ISSN журнала: 23806508
Место издания: NEW YORK
Издатель: IEEE