AEROSPACE CHINA

中国航天科技集团有限公司主管

中国航天系统科学与工程研究院主办

ISSN 1671-0940

CN 11-4673/V

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AEROSPACE CHINA ›› 2017, Vol. 18 ›› Issue (2): 31-39.doi: 10.3969/j.issn.1671-0940.2017.02.004

• 综述 • 上一篇    下一篇

FY-4 Meteorological Satellite

  

  • 出版日期:2017-06-15 发布日期:2019-11-28

FY-4 Meteorological Satellite

  1. Shanghai Academy of Spaceflight Technology, Shanghai 201109
  • Online:2017-06-15 Published:2019-11-28
  • About author:DONG Yaohai (1966 - ), graduated from the Harbin Institute of Technology. Dong is standing member of the Science and Technology Committee, SAST. He is the leader of China second generation LEO meteorological satellite engineering – FY-3, who has ever participated in the whole development of China first generation LEO meteorological satellite – FY-1 A, B, C and D. He is the chief designer for FY-4 meteorological satellite.

Abstract: FY-4 is the second generation of Chinese geostationary satellite for quantitative remote sensing meteorological application. The detection efficiency, spectral bands, spatial and time resolution have been greatly improved with respect to those of first generation, as well as the radiometric calibration and sensitivity. The combination of multichannel detection and vertical sounding was first realized on FY-4, because both the Advanced Geostationary Radiation Imager (AGRI) and Geostationary Interferometric Infrared Sounder (GIIRS) are on the same spacecraft. The main performance of the payloads including AGRI, GIIRS and Lightning Mapping Imager, and the spacecraft bus are presented, the performance being equivalent to the level of the third generation meteorological satellites in Europe and USA. The acquiring methods of remote sensing data including multichannel and high precision quantitative observing, imaging collection of the ground and cloud, vertical observation of atmospheric temperature and moisture, lightning imaging observation and space environment detection are shown. Several innovative technologies including high accuracy rotation angle detection and scanning control, high precision calibration, micro vibration suppression, unified reference of platform and payload and on-orbit measurement, real-time image navigation and registration on-orbit were applied in FY-4.