Simulation studies for the NASA scatterometer on NROSSA methodology for the design of a spaceborne radar scatterometer system configuration which includes parameters such as antenna pointing angles, antenna azimuth angles, antenna polarization, and measurement swath locations is presented. The methodology was applied to the NASA Scatterometer (NSCAT). The performance tradeoff studies on the NSCAT system configuration required development of a computer simulation to estimate wind retrieval accuracy for a given system configuration; and a series of metrics to quantify the simulation results and allow direct comparison of the performance for different configurations.
Document ID
19870008785
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chi, Chong-Yung (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Aroian, R. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Li, Fuk K. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1986
Publication Information
Publication: ESA Proceedings of the 1986 International Geoscience and Remote Sensing Symposium (IGARSS '86) on Remote Sensing: Today's Solutions for Tomorrow's Information Needs, Volume 3