Journal of Deep Space Exploration >

2022 , Vol. 9 >Issue 2: 183 - 190

DOI: https://doi.org/10.15982/j.issn.2096-9287.2022.20210099

Research Papers

X-Band TT&C Design in Launch and Early Orbit Phase for Chang’ E-5

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  • 1. Beijing Institute of Tracking and Telecommunication Technology，Beijing 100094，China;
    2. China Satellite Marine Track & Control Department， Jiangyin 214431， China;
    3. Xi’ an Satellite Control Center， Xi’ an 710043， China

Received date: 23 Nov 2021

Revised date: 06 Jan 2022

Published date: 20 May 2022

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Abstract

Due to advantage of high measurement accuracy and less interfere. X band TT&C had been the main frequency band in lunar and deepspace exploration. Chang’E-5 used X band TT&C in launch phase first time. Compared with S band, X band had the shortage of wider target dynamic range、narrower antenna beam，and shorter system acquisition time. Furthermore Long March 5 rocket used narrow window multi-orbit launch plan. Both of them asked for higher requirements in launch phase quick acquisition, TT&C ship position determination，first acquisition of ground station after separation. In view of the difficulties of narrower ground antenna beam, wider frequency dynamic range and wider receiver bandwidth of explorer in the launch and early orbit phase for Chang’E-5， an overall plan of the X-band was designed by using such methods as analyzing ship position covered by feature points，Doppler preset fast scan capture and cooperated backup of deep-space stations between ESA (European Space Agency) and Kuru，which effectively reduced the risk of implementation and ensured the success of the mission. Chang’E-5 mission has laid a foundation for the overall design and construction planning of the future lunar and deep space TT&C mission.

Key words： Chang’E-5; launch and early orbit phase; two-way acquisition; TT&C general design

Cite this article

LI Haitao, CHENG Cheng, HUANG Lei, CHEN Shaowu, LI Yubo, QIANG Li, KANG Kai . X-Band TT&C Design in Launch and Early Orbit Phase for Chang’ E-5[J]. Journal of Deep Space Exploration, 2022 , 9(2) : 183 -190 . DOI: 10.15982/j.issn.2096-9287.2022.20210099

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