NASDA (National Space Development Agency of Japan) has been updating the long term Earth observation scenario.
In the latest scenario, it was classified into the following; global observation, regional land observation, diurnal cycle observation, geostationary observation and experimental flight for newly developed sensors. ADEOS, ADEOS-II for global observation, ALOS for regional land observation and TRMM for diurnal cycle observation have been carried forward actually.
ADEOS-II (ADVANCED EARTH OBSERVATION SATELLITE-II) is a post-ADEOS polar orbiting satellite, major objectives of which are to observe the global environment change by international cooperation and to develop satellite remote-sensing technology.
The mission of ADEOS-II is to obtain earth science data regarding global water and energy cycling and carbon cycling. In order to achieve this mission, in addition to two instruments, AMSR and GLI, developed by NASDA, three instruments, ILAS-Il, SeaWinds and POLDER, are to be developed and delivered to ADEOS-II by Environment Agency of Japan, NASA/JPL, CNES, respectively.
The primary objectives of the AMSR(Advanced Microwave Scanning Radiometer) are to obtain the physical content concerning water cycling. AMSR has the capability of measuring dual polarized microwave radiation from the earth's atmosphere and surface at 8 frequencies in the region from 6.9 GHz to 89 GHz with 1600 km of swath width and 5 to 50 km spatial resolution.
AMSR scans the surface with the mechanical rotation of 2 m aperture antenna to achieve the constant incident angle and the wide swath width.
The primary objectives of the GLI (GLobal Imager) are to obtain the physical content concerning carbon and water cycling and primary ocean production.
GLI measures the reflectance and radiation from land and sea surfaces and atmosphere with 36 channels in the spectrum range from 375 nm to 12.5, um, 1600 km of swath width and 1 km and 250 m spatial resolution.
GLI scans the surface in the direction of cross-track by the mechanical rotation of mirror both side of which will be used. In the direction of along-track GLI has 12 detectors arrays, therefore rotation velocity of the mirror will be reduced. Because of this the integration time will be made long and accuracy will be improved. Now these instruments are in the phase of manufacturing and test of engineering model, to validate the flight design. And the RA (Research Announcement) were issued.
View full abstract