Journal of Atmospheric and Environmental Optics, Volume. 18, Issue 4, 295(2023)
Engineering design and in-orbit performance evaluation of polarization crossfire suite onboard the hyperspectral observation satellite
Fig. 1. Payloads configuration of hyperspectral observation satellite[16]
Fig. 2. Schematic diagram of the working principle of polarization crossfire[3]
Fig. 3. Schematic diagram of second pulse timing implementation scheme
Fig. 6. Results of synchronous observation and acquisition time difference in orbit
Fig. 7. Heat map of correlation between DPC and POSP field of view matching at different pixel positions in DPC
Fig. 8. In-orbit cross-calibration results of DPC and POSP of the hyperspectral observation satellite.(a) 443 nm; (b) 490 nm; (c) 670 nm; (d) 865 nm
Fig. 9. Linear fitting and statistical distribution results of polarization of DPC and POSP[12]. (a) 490 nm; (b) 670 nm; (c) 865 nm
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Miaomiao ZHANG, Yuan WEN, Sifeng ZHU, Yanqing XIE, Yingjie LI, Yunduan LI, Jin HONG, Zhenhai LIU, Donggen LUO, Maoxin SONG, Yi WANG. Engineering design and in-orbit performance evaluation of polarization crossfire suite onboard the hyperspectral observation satellite[J]. Journal of Atmospheric and Environmental Optics, 2023, 18(4): 295
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Received: Mar. 17, 2023
Accepted: --
Published Online: Aug. 24, 2023
The Author Email: HONG Jin (hongjin@aiofm.ac.cn)