Please use this identifier to cite or link to this item: http://hdl.handle.net/2122/9796
AuthorsPierdicca, N.* 
Bignami, C.* 
Roca, M.* 
Féménias, P.* 
Fascetti, M.* 
Mazzetta, M.* 
Loddo, C.N.* 
Martini, A.* 
Pinori, S.* 
TitleTransponder calibration of the Envisat RA-2 altimeter Ku band sigma naught
Issue Date2013
Series/Report no./51 (2013)
DOI10.1016/j.asr.2012.12.014
URIhttp://hdl.handle.net/2122/9796
KeywordsRadar Altimetre
Transponder
External Calibration
Backscattering
Subject Classification05. General::05.04. Instrumentation and techniques of general interest::05.04.99. General or miscellaneous 
AbstractAlthough the history of spaceborne altimeters goes back to the early seventies, the absolute calibration of the backscattering coefficient has never been deeply investigated. This information has been primarily used to infer the wind speed via an empirical model, and the intercalibration among different satellite altimeters has revealed to be suitable for this purpose, being the wind retrieval based on an empirical relationship. As far as Ku band system is concerned, the sigma naught absolute calibration of the Envisat altimeter (RA-2) has been performed using an active reference target provided by a transponder. This has been exploited during the 6-month Commissioning phase to generate early calibration results. In order to monitor the RA-2 backscatter calibration during the Envisat lifetime, a continuous calibration effort has been carried out by operating the transponder as much as possible. This paper aims to review the entire effort for calibrating the RA-2 sigma naught measurements, which lasted for almost seven years. It presents in detail the adopted methodology and the final outcome of the activity, providing the users with the correction (bias) to get the calibrated sigma naught and analyzing its stability during almost the entire Envisat lifetime. Specifically, it is concluded that the RA-2 backscatter measurements were quite stable, even if a bias of about 1 dB should be considered with respect to the actually released product. Some small changes in the bias as function of time can be identified during most of the Envisat lifetime, consisting in a slight increase in the first two years, followed by a more stable period and a final drop observed at the end of 2009, until the conclusion of the calibration activity (corresponding to the change in Envisat orbit).
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