FY-4 (FengYun-4) Geostationary Meteorological Satellite Series
FY-4 is CMA's (China Meteorological Administration) second-generation three-axis stabilized, geostationary meteorological satellite series, under development by CAST (China Academy of Space Technology). Two variants of spacecraft of the FY-4 (FenYun means "winds and clouds or storm" in Chinese) program are in planning, with one carrying optical sensors and the other carrying microwave sensors.
Compared to the current FY-2 geostationary meteorological satellite series, the performance of the FY-4 series has been considerably improved in terms of data amount, network transmission bandwidth, product type and quantity and archiving data and applications. The new generation FY-4 satellites are designed with an enhanced imagery scanning capability, desirable for monitoring small and medium scale weather systems. FY-4 is enabled with vertical atmospheric sounding and microwave detection capabilities to address 3D remote sensing at geostationary altitudes. The new FY-4 series is also enabled with solar observations for EUV (Extreme Ultraviolet) and X-ray monitoring, in a bid to enhance China's space weather watch and warning capability. 1)
Based on user requirements and technical feasibility, the missions of the FY-4 series include imagery, sounding, lightning mapping, and space environment monitoring. HRIT (High Rate Information Transmission), LRIT (Low Rate Information Transmission) data transmission, and DCP (Data Collection Platform) services are available for users. 2) 3) 4) 5)
In 2015, the Chinese government approved the NSIP (National Space Infrastructure Plan) covering also the meteorological program of LEO and GEO missions up to 2025. 6)
The geostationary FenYun-4 series consists of seven spacecraft:
• FY-4A (2016-2021)
• FY-4B (2018-2025)
• FY-4C (2020-2027)
• FY-4D (2023-2030)
• FY-4E (2027-2034)
• FY-4F (2030-2037)
• FY-4G (2033-2040)
Next to the first FY-4 missions with optical payloads, CMA is also planning for FY-4 missions with MW (Microwave) payloads as shown in Figure 1.
FY-4 Optical Series
The optical variant will include two satellites: FengYun-4 ‘East', which will cover a region including western China, the Indian Ocean, the Red Sea and the Middle East; and FengYun-4 ‘West', which will cover a region including middle and eastern China and the Pacific. The microwave variant FengYun-4 will cover China and its peripheral areas. The FY-4A mission is considered a pre-operational (pathfinder, or R&D) mission with the follow-on FY-4B, -4C spacecraft are considered operational missions. 7) 8) 9) 10) 11) 12) 13)
The main tasks are described as follows:
- a) To obtain the multi-spectrum and high-accurate quantitative images of the earth and clouds;
- b) To measure the humidity parameter of atmosphere;
- c) To enhance the ability of detecting the space weather and environment;
- d) To collect various earth environmental parameter;
- e) To broadcast images, weather products, and the devastating weather forecasting.
Table 1: Comparison of FY-4 and FY-2 key mission parameters
The FY-4 series of geostationary spacecraft are being designed and developed by CASC/SAST (China Aerospace Science and Technology Corporation/Shanghai Academy of Space Technology). The SAST-5000 bus features an attitude determination system relying on star trackers, inertial measurement systems and Earth/Sun sensors with reaction wheels acting as the primary attitude actuator, achieving a high pointing accuracy of 3arcsec at low jitter to keep the satellite in a precise Earth-pointed attitude. Internal communications on the satellite use the 1553B communications standard and high-speed SpaceWire which supports the data rates required by the instruments and allows for easy integration. Downlink of raw instrument data is completed in real time via a high-speed X-band terminal operating at 7.500 GHz.
1) Launch mass: ~5300 kg
2) Spacecraft stabilization: Three-axis stabilization
3) Attitude accuracy: 3 arcsec
4) Onboard communication bus: 1553B+SpaceWire
5) Raw data transmission : X-band
6) Output power: ≥ 3.2 kW
7) Spacecraft design life: 7 years.
Figure 2: Illustration of the FY-4A prototype spacecraft (image credit: CMA/NSMC, Ref. 12)
Launch: The FY-4A spacecraft was launched on December 10, 2016 (16:11:00 UTC) on a Long March 3B vehicle from the XSLC (Xichang Satellite Launch Center) in the Sichuan Province of southwest China. 14) 15)
Orbit: Geostationary orbit, altitude = 35786 km, longitude = 99.5º E.
• February 28, 2017: FengYun-4A, the first of China's second-generation geostationary orbiting weather satellites, has sent its first collection of images and data. SASTIND (State Administration of Science, Technology and Industry for National Defence) and CMA (China Meteorological Administration) published the images and data on Feb. 27, signaling the successful upgrade of China's meteorological system. 16) 17)
- The composite image of Figure 3 was acquired by the instruments AGRI (Advanced Geosynchronous Radiation Imager) and GIIRS (Geostationary Interferometric Infrared Sounder).
- "We achieved a very successful engineering development. Four major payload devices of the FengYun-4 satellite started up smoothly and captured the first batch of data. The quality of the images is great. The information gained is up to what is expected in terms of quality and is qualified for use," said Tian Yulong, chief engineer of SASTIND.
Sensor complement of FY-4A configuration: (AGRI, GIIRS, GLI/(LMI), SEP, DCS)
The sensor complement of the new generation satellites are designed with an enhanced imagery scanning capability, desirable for monitoring small and medium scale weather systems. It is enabled with vertical atmospheric sounding and microwave detection capabilities to address 3D remote sensing at high altitudes. It is also enabled with solar observations for extreme ultraviolet and X-rays, in a bid to enhance China's space weather watch and warning capability. 18)
AGRI (Advanced Geosynchronous Radiation Imager)
AGRI is of ABI (Advanced Baseline Imager) heritage to be flown on GOES-R of NASA/NOAA (launch of GOES-R on Nov. 19, 2016). AGRI is being constructed by Harris Corporation, formerly ITT Exelis of Fort Wayne, IN, USA. In May 2015, Harris Corp. of Melbourne, FL. acquired Exelis Inc. of Fort Wayne, IN. AGRI uses an off-axis telescope, two scan mirrors, 216 detectors in 14 spectral bands, and full-path on-orbit calibration. 19)
AGRI is replacing the S-VISSR sensor, flown on the FY-2A to H series. AGRI is the primary instrument of FY-4A, has 14 channels and two observation modes. The temporal resolutions are 1 - 5 minutes over a regional domain and 15 minutes over the full-disk domain.
AGRI is a multispectral imager with a two-axis scanning geometry, vastly expanding previous capabilities by adding spectral channels, improving spectral and spatial resolution of imagery, and employing a much faster data acquisition scheme.
GIIRS (Geostationary Interferometric Infrared Sounder)
GIIRS, developed by National Space Science Center of CAS, will be the main payload on board of FY-4A satellite to monitor and measure internal constitution and precipitation parameters of the atmosphere cloud cluster. 22)
Table 3: Key parameters of the GIIRS instrument
GIIRS can be used for vertical atmospheric sounding and it is the first high-resolution sounding sensor onboard the geostationary satellite. There are two observation modes of GIIRS. One mode is designed for China area, whose temporal resolution is 55 minutes and the coverage is 4500 x 4500 km. The other observation mode is mesoscale mode, whose temporal resolution is 30 minutes and the coverage is 1000 x 1000 km.
GIIRS is a MWIR (Mid-Wave Infrared)/TIR (Thermal Infrared) sounder with large detector arrays for simultaneous sounding of a larger area plus visible coverage support for cloud detection. The instrument operates by stepping dual scanning mirrors to subsequent scan positions with a specific dwell time over each location for data acquisition. On FY-4A, GIIRS covers 538 TIR channels and 375 MWIR channels, to be expanded to 1,188 detectors on the operational missions of FY-4B and forward.
The GIIRS detectors employ a deep data quantization of 13 bit and active coolers keep the 32 x 4 focal plane at a constantly low temperature for dark current reduction.
Data delivered by GIIRS is used to for atmospheric temperature profiles, cloud top height and temperature, sea surface temperature, specific humidity profiles, integrated water vapor measurements, cloud cover maps, land surface temperature, horizontal winds, total column ozone, and cloud type discrimination.
GLI (Geostationary Lightning Imager) — also called LMI (Lightning Mapper Imager)
The FY-4 spacecraft will carry the GLI (Geostationary Lightning Imager), which is the first lightning detection sensor on China's satellites. The GLI will be used to observe regional lightning activity in China. The GLI products will be used in forecasting and warning of convection precipitation, and studying of Earth's electric field. 23)
The objectives of the FY-4 GLI instrument are to measure the total lightning (both intracloud and cloud-to-ground) activity within its FOV (Field of View) continuously during both day and night. It will provide measurement with a resolution of 7.8 km at the subsatellite point and full disk continuously observed with a time resolution of about 2 ms. The CCD (Charge-Coupled Device) camera will operate at 777.4 nm to count flashes and measure their intensity. For that 777.4 nm is within the solar reflective band, a vicarious calibration using DCCs (Deep Convective Clouds) as stable targets is applicable.
The GLI 400 x 600 pixel CCD focal plane will stare continuously at storms from the FY-4 satellite. The GLI shall have a continuous monitoring capability across a coverage (9,000 km diagonal field-of-view) with a near-uniform round sample 8-14 km pixel footprint resolution.
Table 4: Specification of the GLI
Figure 4: FOV view from the FY-4 GLI superimposed on one month (July, 2008) of lightning observations from the NASA LIS (Lightning Imager Sensor) on board the Tropical Rainfall Measuring Mission (TRMM/LIS) LEO satellite (image credit: CMA, NASA)
SEP (Space Environment Monitoring Package)
Monitoring of charged particles at platform level. Package of instruments for energetic particle detectors. Set of counters for electrons (0.4-4 MeV) and protons (1-165 MeV).
• High-energy Proton Detector: 8 channels in the energy range of 1-165 MeV; the FOV is conical at 60º.
• High-energy Electron Detector: 9 channels in the energy range of 0.4 - 4 MeV; the FOV is conical at 25º.
• Package of instruments including a FGM (Flux Gate Magnetometer), and radiation dosimeter and surface charging sensors. Dynamic range of FGM: ±0.01 to ±600 nT for each component, with resolution ±0.06 @ maximum of the dynamics.
DCS (Data Collection System)
Data collection from DCPs (Data Collection Platforms) in the ground segment. Two types of DCPs will be served: either regional, or international (i.e. migrating across the field of view of more geostationary satellites).
Figure 5: New FY-4A ground segment: Elements & Layout (image credit: NSMC/CAS) 24)
FY-4A will provide 28 baseline products as shownin Table 5. All algorithm design and development have already been completed. The next step plans to use simulation data to validate the reliability of each algorithm.
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23) Dongjie Cao, Fuxiang Huang, Xiushu Qie, "Development and Evaluation of detection algorithm for FY-4 Geostationary Lightning Imager (GLI) measurement," XV International Conference on Atmospheric Electricity, 15-20 June 2014, Norman, Oklahoma, USA, URL: http://www.nssl.noaa.gov/users/mansell/icae2014/preprints/Cao_59.pdf
24) Caiying Wei, "Updates on Chinese Meteorological Satellite Programs," 6th Asia/Oceania Meteorological Satellite Users' Conference, Tokyo, Japan, Nov. 10, 2015, 2nd ISCC Meeting was held during Oct. 14-17, 2015, Beijing, China, URL: http://www.data.jma.go.jp/mscweb/en/aomsuc6_data/oral/s01-05.pdf
The information compiled and edited in this article was provided by Herbert J. Kramer from his documentation of: "Observation of the Earth and Its Environment: Survey of Missions and Sensors" (Springer Verlag) as well as many other sources after the publication of the 4th edition in 2002. - Comments and corrections to this article are always welcome for further updates (email@example.com).