9 June 2006 The preliminary system parameters design for RICESAT
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Proceedings Volume 6200, Remote Sensing of the Environment: 15th National Symposium on Remote Sensing of China; 620005 (2006) https://doi.org/10.1117/12.681143
Event: Remote Sensing of the Environment: 15th National Symposium on Remote Sensing of China, 2005, Guiyan City, China
Abstract
The user requirement for the rice satellite (RICESAT) is analyzed, basing on the radar backscattering coefficient characteristic of rice crops. The orbital elements of RICESAT are selected. The payload of RICESAT was designed as C-band synthetic aperture radar (SAR) system with HH and VV polarization, operating in Strip Map mode or Scan SAR mode. The orbital elements of RICESAT are selected, and the key parameters of the SAR payload are designed. The computer simulation results are presented in the paper, which demonstrates the preliminary feasibility of RICESAT.
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Jie Chen, Jie Chen, Huaping Xu, Huaping Xu, Chunsheng Li, Chunsheng Li, Yinqing Zhou, Yinqing Zhou, } "The preliminary system parameters design for RICESAT", Proc. SPIE 6200, Remote Sensing of the Environment: 15th National Symposium on Remote Sensing of China, 620005 (9 June 2006); doi: 10.1117/12.681143; https://doi.org/10.1117/12.681143
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