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
来源：
INSTRUMENTATION, MEASUREMENT, CIRCUITS AND SYSTEMS | 2012年 / 127卷
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
  • [41] SHARAD sounding radar on the Mars Reconnaissance Orbiter
    Seu, Roberto
    Phillips, Roger J.
    Biccari, Daniela
    Orosei, Roberto
    Masdea, Arturo
    Picardi, Giovanni
    Safaeinili, Ali
    Campbell, Bruce A.
    Plaut, Jeffrey J.
    Marinangeli, Lucia
    Smrekar, Suzanne E.
    Nunes, Daniel C.
    JOURNAL OF GEOPHYSICAL RESEARCH-PLANETS, 2007, 112 (E5)
  • [42] Structural attitudes of large scale layering in Valles Marineris, Mars, calculated from Mars Orbiter Laser Altimeter data and Mars Orbiter Camera imagery
    Fueten, F
    Stesky, RM
    MacKinnon, P
    ICARUS, 2005, 175 (01) : 68 - 77
  • [43] Trajectory design for the Mars Reconnaissance Orbiter mission
    Halsell, CA
    Bowes, AL
    Johnston, MD
    Lyons, DT
    Lock, RE
    Xaypraseuth, P
    Bhaskaran, SK
    Highsmith, DE
    Jah, MK
    SPACEFLIGHT MECHANICS 2003, PTS 1-3, 2003, 114 : 1591 - 1606
  • [44] MARS ORBITER INSERTION BY USE OF ATMOSPHERIC DECELERATION
    OKHOTSIMSKY, DE
    GOLUBIEV, YF
    SIKHARULIDZE, YG
    ACTA ASTRONAUTICA, 1978, 5 (10) : 765 - 780
  • [45] Mission automation and autonomy for the Mars Orbiter Mission
    Karidhal, Ritu
    Harinath, Nandini
    Robert, P.
    Kesavaraju, V.
    CURRENT SCIENCE, 2015, 109 (06): : 1070 - 1075
  • [46] Mars Orbiter Mission spacecraft and its challenges
    Arunan, S.
    Satish, R.
    CURRENT SCIENCE, 2015, 109 (06): : 1061 - 1069
  • [47] Electromagnetic Compatibility of Mars Orbiter Mission Spacecraft
    Raghavaiah, Vaddi
    Sowjanya, P.
    Mini, R. L.
    Murthy, P. V. N.
    Muniraja, S. M.
    Renuka, R.
    Murali, G. K. Rama
    Binu, D.
    Sankaranarayanan, Santhi
    Kumar, V. Senthil
    Srinivas, B. S.
    Hariharan, V. K.
    Srinivasan, V. V.
    2014 IEEE INTERNATIONAL MICROWAVE AND RF CONFERENCE (IMARC), 2014, : 209 - 212
  • [48] PLANETARY SCIENCE Mars orbiter to sniff for methane
    Hand, Eric
    SCIENCE, 2016, 351 (6278) : 1122 - 1123
  • [49] IPL PROCESSING OF VIKING ORBITER IMAGES OF MARS
    RUIZ, R
    ELLIOTT, D
    YAGI, G
    POMPHREY, R
    POWER, M
    FARRELL, KW
    LORRE, J
    BENTON, W
    DEWAR, R
    CULLEN, L
    TRANSACTIONS-AMERICAN GEOPHYSICAL UNION, 1977, 58 (08): : 830 - 830
  • [50] COMPARISON OF VISUAL IMAGING SYSTEMS FOR A MARS ORBITER
    SEAMAN, LT
    KLEMAS, V
    JOURNAL OF THE SOCIETY OF MOTION PICTURE TELEVISION ENGINEERS, 1970, 79 (01): : 7 - &
12345