Feasibility Study of USO's Stability in Mars Exploration

被引：0

作者：

Wang Zhen ^{[1
]}

Shang Kun

Wang Na ^{[1
]}

Ping Jin Song

机构：

[1] Chinese Acad Sci, Xinjiang Astron Observ, Urumqi 830011, Peoples R China

来源：

2011 INTERNATIONAL CONFERENCE ON AEROSPACE ENGINEERING AND INFORMATION TECHNOLOGY (AEIT 2011) | 2011年

关键词：

YingHuo-1; Ultra Stable Oscillator; frequency standard;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The launch schedule of China's first Mars orbiter "YingHuo-1" is about 2011, to solve the tracking problem, the kernel payload of "YingHuo-1" is Ultra Stable Oscillator used for frequency standard, the transmitter generate a standard downlink signal. The ground astronomical VLBI system will be used to receive the radio signal. In this article, the experimental data of YingHuo-1's Ultra Stable Oscillator was processed, and result shows the frequency stability is about 10(12), which can support for the real-time precise orbit determination.

引用

页码：40 / 44

页数：5

共 8 条

[1] STATISTICS OF ATOMIC FREQUENCY STANDARDS
ALLAN, DW
[J]. PROCEEDINGS OF THE INSTITUTE OF ELECTRICAL AND ELECTRONICS ENGINEERS, 1966, 54 (02): : 221 - &
[2] A digital open-loop Doppler processing prototype for deep-space navigation
Jian NianChuan
Shang Kun
Zhang SuJun
Wang MingYuan
Shi Xian
Ping JingSong
Yan JianGuo
Tang GeShi
Liu JunZe
Qiu Shi
Fung Lai-Wo
Zhang Hua
Wang Zhen
Gou Wei
[J]. SCIENCE IN CHINA SERIES G-PHYSICS MECHANICS & ASTRONOMY, 2009, 52 (12): : 1849 - 1857
[3] Phobos-Grunt: Russian sample return mission
Marov, MY
Avduevsky, VS
Akim, EL
Eneev, TM
Kremnev, RS
Kulikov, SD
Pichkhadze, KM
Popov, GA
Rogovsky, GN
[J]. MERCURY, MARS AND SATURN, 2004, 33 (12): : 2276 - 2280
[4] Ping Jin-Song, 2009, Wuli, V38, P779
[5] Ruggier C.J, 2000, JPL PUBLICATION, P5
[6] Shang Kim, 2009, Wuli, V38, P799
[7] [王震 Wang Zhen], 2010, [天文学进展, Progress in Astronomy], V28, P424
[8] Yuen J. H., 1983, DEEP SPACE TELECOMMU, P123

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