Performance and application of the Chinese satellite-to-satellite tracking gravimetry system

被引:6
|
作者
Xiao, Yun [1 ,2 ]
Yang, Yuanxi [1 ,2 ]
Pan, Zongpeng [1 ,2 ]
Liu, Xiaogang [1 ,2 ]
Sun, Zhongmiao [1 ,2 ]
机构
[1] Xian Res Inst Surveying & Mapping, Xian 710054, Peoples R China
[2] State Key Lab Geo Informat Engn, Xian 710054, Peoples R China
来源
CHINESE SCIENCE BULLETIN-CHINESE | 2023年 / 68卷 / 20期
关键词
satellite gravimetry; satellite-to-satellite tracking; Chinese gravimetry satellite; Earth's gravity field; GRAVITY-FIELD RECOVERY;
D O I
10.1360/TB-2022-1057
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
The first pair of satellite to satellite tracking gravimetric satellites from China (Chinese gravimetric mission) was successfully launched at the end of 2021. It adopts a hybrid measurement system of high-low satellite to satellite tracking (HL-SST) and low-low satellite-to-satellite tracking (LL-SST) to obtain measurements of the global gravity field and its time-varying information, which can be used to study groundwater changes, glacier ablation, space micro-gravity fluctuations, ocean tides, earthquakes, etc. The data can be used for scientific research and engineering construction in the fields of natural resources, ocean, aerospace, and water conservancy, et al. The Chinese gravimetric satellite platform is designed to be ultra-silent, ultra-stable and ultra-accurate. In-orbit test results show that the working state of the platform is normal and all indicators meet the design requirements with margin. This significantly improves the development level of the satellite platform and the level of space micro-gravity measurement, and will expand the prospect for scientific applications in various fields. Firstly, this paper briefly introduces the Chinese gravimetric satellite and discusses the technical characteristics of the integrated design of the satellite platform. This platform provides an environment with low vibrations, stable temperature, precise pointing and tiny deformation of the structure for the whole satellite, and ensures that the payloads of the inter-satellite ranging system and electrostatic suspension accelerometer work in suitable conditions. Secondly, the characteristics and performance figures of the inter-satellite ranging system, electrostatic suspension accelerometer, BDS/GPS common mode receiver and star sensors are analyzed. The inter-satellite ranging system is based on K/Ka-band ranging (KBR) in the dual-one way ranging configuration with stable performance and ranging noise level being better than 3 mu m/Hz(1/2) in the frequency band of 0.025-0.1 Hz. The accelerometer works with electrostatic suspension mode, which is highly sensitive to the residual thrust of the attitude control thruster, switching of the magnetic torquer and other small vibrations. The spectrum analysis shows its high-sensitive axis noise level is being 3x10(-10) m/(s(2) Hz(1/2)) near the frequency 0.1 Hz, and being 1x10(-9) m/(s(2) Hz(1/2)) for the less-sensitive axis. The three star sensors are designed integrally with the tiny deformation structure. To verify the attitude measurement accuracy, the angles between star sensor boresights arecalculated, then the average of the angles is removed, the standard deviation (STD) of residuals is better than 3 ''. The center of mass detection and adjustment system reaches the accuracy level of 100 mu m. The BDS/GPS common mode receiver observers BDS-3 signals and GPS signals simultaneously. The data from the BDS/GPS receiver are used for satellite precise orbit determination (POD) and time synchronization. The achieved accuracy of the satellite orbits is better than 2 cm determined from a comparison of the kinematic and reduced-dynamic orbits. Comparing the baseline of the KBR system with the POD yields RMS residuals of less than 1 mm. Finally, the time-varying Earth gravity field recovery is performed from April 1, 2022 to August 30, 2022 using the in-orbit satellite data, such as KBR data, attitude and orbit data as well as with measurements of non-gravitational accelerations obtained from accelerometers. The time-varying Earth gravity model with a maximum degree of 60 is named Chinese Earth Gravity Field Model 22-01 (CEGM22S-01), and it is converted into an equivalent water height which can be applied to Amazon terrestrial water storage monitoring. The results show that the model can well characterize global hydrological changes, such as the mass loss of Greenland and the terrestrial water storage changes of the Amazon River, and correlates strongly with the results of GRACE Follow-On with the root mean square (RMS) difference of 2 cm in global equivalent water height. Subsequently, with the accumulation of further satellite telemetry, the continuous time-varying gravity field, space atmospheric density, space horizontal ionosphere, space magnetic field and other products can be produced, which will provide abundant information services for the fields of geophysics, geodesy, earthquake, water resources environment, ocean, national defense, etc. The Chinese gravimetric mission will continue to serve relevant scientific research and engineering applications and continue to reveal more scientific application values.
引用
收藏
页码:2655 / 2664
页数:10
相关论文
共 41 条
  • [1] Tongji-Grace02s and Tongji-Grace02k: High-Precision Static GRACE-Only Global Earth's Gravity Field Models Derived by Refined Data Processing Strategies
    Chen, Qiujie
    Shen, Yunzhong
    Francis, Olivier
    Chen, Wu
    Zhang, Xingfu
    Hsu, Houze
    [J]. JOURNAL OF GEOPHYSICAL RESEARCH-SOLID EARTH, 2018, 123 (07) : 6111 - 6137
  • [2] [陈秋杰 Chen Qiujie], 2016, [测绘学报, Acta Geodetica et Cartographica Sinica], V45, P396
  • [3] [陈威 Chen Wei], 2017, [科学通报, Chinese Science Bulletin], V62, P2116
  • [4] Gravitational perturbation theory for intersatellite tracking
    Cheng, MK
    [J]. JOURNAL OF GEODESY, 2002, 76 (03) : 169 - 185
  • [5] Understanding data noise in gravity field recovery on the basis of inter-satellite ranging measurements acquired by the satellite gravimetry mission GRACE
    Ditmar, Pavel
    da Encarnacao, Joao Teixeira
    Farahani, Hassan Hashemi
    [J]. JOURNAL OF GEODESY, 2012, 86 (06) : 441 - 465
  • [6] GOCE: ESA's first Earth Explorer Core mission
    Drinkwater, MR
    Floberghagen, R
    Haagmans, R
    Muzi, D
    Popescu, A
    [J]. SPACE SCIENCE REVIEWS, 2003, 108 (1-2) : 419 - 432
  • [7] Feng W, 2013, THESIS U CHINESE ACA
  • [8] Forste Christoph, 2014, GFZ
  • [9] Hsu H Z, 2012, SCI SIN TERRAE, V42, P843
  • [10] [金双根 Jin Shuanggen], 2012, [科学通报, Chinese Science Bulletin], V57, P3484