DocumentCode :
144408
Title :
In-orbit correction and optimization design of the calibration assembly for HY-2 microwave radiometer
Author :
Yanming Li ; Jun Li ; Taiyang Hu ; Chongdi Duan ; Wenxin Chen ; Weining Lei
Author_Institution :
China Acad. of Space Technol. (Xi´an), Xi´an, China
fYear :
2014
fDate :
13-18 July 2014
Firstpage :
5183
Lastpage :
5186
Abstract :
The HY-2 microwave radiometer containing nine channels, whose operational frequencies range from 6.6 GHz to 37 GHz, is one of the four microwave payloads deployed on the HY-2 satellite. After launch, both the hot blackbody counts and cold sky counts are processed before producing the Level 1b data, and the influence on cold sky observation resulted by main reflector draws special attention. Moreover, it is verified that the fluctuation mentioned above can be up to 2.4 K at 6.6 GHz, and this effect is corrected through processing the acquired data. In view of the realistic problem, some corresponding improvements have been carried out in the subsequent satellite´s design phase. This paper describes characteristics of the instrument, and the corrections to cold sky counts are also provided. Finally, the optimization design is presented and evaluated.
Keywords :
artificial satellites; assembling; calibration; celestial mechanics; microwave detectors; millimetre wave detectors; optimisation; radiometers; HY-2 microwave radiometer; HY-2 satellite; calibration assembly; cold sky count; cold sky observation; frequency 6.6 GHz to 37 GHz; hot blackbody count; in-orbit correction; level 1b data; optimization design; Calibration; Earth; Microwave radiometry; Microwave theory and techniques; Receivers; Satellite broadcasting; Satellites; Calibration assembly; HY-2 satellite; In-orbit correction; Microwave radiometer; Optimization design;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Geoscience and Remote Sensing Symposium (IGARSS), 2014 IEEE International
Conference_Location :
Quebec City, QC
Type :
conf
DOI :
10.1109/IGARSS.2014.6947666
Filename :
6947666
Link To Document :
بازگشت