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Proceedings Paper

The preliminary system parameters design for RICESAT
Author(s): Jie Chen; Huaping Xu; Chunsheng Li; Yinqing Zhou
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Paper 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.

Paper Details

Date Published: 9 June 2006
PDF: 6 pages
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
Show Author Affiliations
Jie Chen, Beijing Univ. of Aeronautics and Astronautics (China)
Huaping Xu, Beijing Univ. of Aeronautics and Astronautics (China)
Chunsheng Li, Beijing Univ. of Aeronautics and Astronautics (China)
Yinqing Zhou, Beijing Univ. of Aeronautics and Astronautics (China)


Published in SPIE Proceedings Vol. 6200:
Remote Sensing of the Environment: 15th National Symposium on Remote Sensing of China
Qingxi Tong; Wei Gao; Huadong Guo, Editor(s)

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