Expected accuracy of the global gravity field for next GRACE satellite gravity mission

被引:5
|
作者
Ran Jiang-Jun [1 ,2 ]
Xu Hou-Ze [1 ]
Shen Yun-Zhong [3 ,4 ]
Zhong Min [1 ]
Zhang Xing-Fu [5 ]
机构
[1] Chinese Acad Sci, State Key Lab Geodesy & Earths Dynam, Wuhan 430077, Peoples R China
[2] Chinese Acad Sci, Beijing 100049, Peoples R China
[3] Tongji Univ, Coll Surveying & Geoinformat, Shanghai 200092, Peoples R China
[4] Tongji Univ, Ctr Spatial Informat Sci & Sustainable Dev, Shanghai 200092, Peoples R China
[5] Guangdong Univ Technol, Fac Civil & Transportat Engn, Guangzhou 510006, Guangdong, Peoples R China
来源
关键词
Data combination; Range; Range rate; Future satellite gravity mission; Expected accuracy;
D O I
10.6038/j.issn.0001-5733.2012.09.009
中图分类号
P3 [地球物理学]; P59 [地球化学];
学科分类号
0708 ; 070902 ;
摘要
For the technology of low-low satellite to satellite tracking, this paper focuses on a method which combines the precise orbit data with range data or range rate data to recover the global gravity field. It not only can calibrate the initial position error of the two satellites, but also make good use of the low frequency gravity information from the mission. Several simulation scenarios are discussed in this paper. The results are as follows. (1) If the precision of range rate measurement is improved by a factor of ten, the accuracy of global gravity field will be 10.6 times better; (2) The accuracy of the global gravity field will be higher than that of GRACE by a factor of about 121 if we use the following accuracy indexes; the accuracy of range rate, altitude, acceleration, orbit position and the distance between the two satellites is 1.0 x 10(-8) m.s(-1), 300 km, 3.0 x 10(-10) m.s(-2) 0.03 m, and 100 km, respectively. Therefore, we recommend the payloads mentioned above for Chinese future satellite gravity mission.
引用
收藏
页码:2898 / 2908
页数:11
相关论文
共 28 条
  • [1] Baker RML, 1960, SEM M AM ROCK SOC LO, P1220
  • [2] [陈俊勇 Chen Junyong], 2002, [测绘科学, Science of surveying and mapping], V27, P8
  • [3] Colombo OL, 1984, NETHERLANDS GEODETIC, V7, P1
  • [4] Jiang WP, 2003, GEOMATICS INFORM SCI, V28, P104
  • [5] INFERENCE OF VARIATIONS IN THE GRAVITY-FIELD FROM SATELLITE-TO-SATELLITE RANGE RATE
    KAULA, WM
    [J]. JOURNAL OF GEOPHYSICAL RESEARCH, 1983, 88 (NB10): : 8345 - 8349
  • [6] Luo J., 2003, THESIS WUHAN U WUHAN
  • [7] Luo ZC, 1996, THESIS WUHAN U WUHAN
  • [8] ITG-CHAMP01:: a CHAMP gravity field model from short kinematic arcs over a one-year observation period
    Mayer-Gürr, T
    Ilk, KH
    Eicker, A
    Feuchtinger, M
    [J]. JOURNAL OF GEODESY, 2005, 78 (7-8) : 462 - 480
  • [9] Mayer-Gurr T, 2006, THESIS THEORETISCHE
  • [10] Nico S, 2005, EARTH MOON PLANETS, V94, P113