The Stability of USO to Mars Orbiter Influence

被引:0
|
作者
Wang, Zhen [1 ,2 ,3 ]
Shang, Kun [4 ]
Ye, Nan [5 ]
Wang, Na [1 ]
Ping, Jin Song [4 ]
机构
[1] Chinese Acad Sci, Xinjiang Astron Observ, 50 S Sci Rd, Urumqi 830011, Xinjiang, Peoples R China
[2] Chinese Acad Sci, Key Lab Radio Astron, Urumqi 830011, Xinjiang, Peoples R China
[3] Shanghai Key Lab Space Navigat & Posit, Shanghai, Peoples R China
[4] Chinese Acad Sci, Shanghai Astron Observ, Shanghai 200030, Peoples R China
[5] State Key Lab Space Dynam, Xian 710043, Peoples R China
关键词
YingHuo-1; Ultra Stable Oscillator; frequency standard;
D O I
暂无
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
The China's first Mars orbiter "YingHuo-1" (YH-1) will he launched in the near future. To solve the tracking problem of Mars satellite, the kernel payload of Ultra Stable Oscillator (USO) of "YingHuo-1" is used for frequency standard, and the transmitter generates a standard downlink radio signal. The ground astronomical Very Long Baseline Interferometry (VLBI) system will be used to receive the radio signal. In this article, to investigate the mechanism of the tracking accuracy of the orbit detemination of YH-1, the experimental data of YingHuo-1's USO was processed, using Solar-system Model and Orbit Determination (SMOD) software system developed at Xinjing Astronomical Observatory. The real-time precise orbit determination can he supported by the simulation experimental result, when the frequency stability of USO is about 10-12.
引用
收藏
页码:477 / +
页数:2
相关论文
共 50 条
  • [1] The effect of USO stability on one-way Doppler navigation of the Mars Reconnaissance Orbiter
    Highsmith, DE
    SPACEFLIGHT MECHANICS 2002, VOL 112, PTS I AND II, 2002, 112 : 529 - 539
  • [2] Feasibility Study of USO's Stability in Mars Exploration
    Wang Zhen
    Shang Kun
    Wang Na
    Ping Jin Song
    2011 INTERNATIONAL CONFERENCE ON AEROSPACE ENGINEERING AND INFORMATION TECHNOLOGY (AEIT 2011), 2011, : 40 - 44
  • [3] Entry probe stability analysis for the Mars Pathfinder and the Mars PREMIER orbiter
    Dieudonne, W
    Spel, M
    PLANETARY PROBE ATMOSPHERIC ENTRY AND DESCENT TRAJECTORY ANALYSIS AND SCIENCE, 2004, 544 : 205 - 211
  • [4] VIKING TO MARS - ORBITER
    不详
    SKY AND TELESCOPE, 1975, 50 (02): : 90 - 92
  • [5] The mars reconnaissance orbiter mission
    Johnston, MD
    Graf, JE
    Zurek, RW
    Eisen, HJ
    Jai, BH
    2004 IEEE AEROSPACE CONFERENCE PROCEEDINGS, VOLS 1-6, 2004, : 135 - 150
  • [6] The Mars Reconnaissance Orbiter mission
    Johnston, MD
    Graf, JE
    Zurek, RW
    Eisen, HJ
    Jai, B
    2003 IEEE AEROSPACE CONFERENCE PROCEEDINGS, VOLS 1-8, 2003, : 191 - 204
  • [7] The Mars Reconnaissance Orbiter mission
    Johnston, M. D.
    Graf, James E.
    Zurek, Richard W.
    Eisen, Howard J.
    Jai, Benhan
    2005 IEEE Aerospace Conference, Vols 1-4, 2005, : 447 - 464
  • [8] The Mars science orbiter concept
    Deutsch, Marie
    Abilleira, Fernando
    Bell, David
    Chodas, Jan
    Edwards, Chad
    Harmon, Corey
    Kerridge, Stuart
    Kinsey, Robert
    Komarek, Tom
    Lisman, Doug
    Lopez, Saturnino
    Vozoff, Joanne
    Willacy, Karen
    Winterhalter, Daniel
    2008 IEEE AEROSPACE CONFERENCE, VOLS 1-9, 2008, : 176 - +
  • [9] Landers and orbiter make for Mars
    不详
    ASTRONOMY & GEOPHYSICS, 2011, 52 (06) : 8 - 9
  • [10] The Mars Reconnaissance Orbiter Mission
    Graf, JE
    Zurek, RW
    Eisen, HJ
    Jai, B
    Johnston, MD
    DePaula, R
    ACTA ASTRONAUTICA, 2005, 57 (2-8) : 566 - 578