2005
DOI: 10.1109/tgrs.2004.840667
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MIRAS reference radiometer: a fully polarimetric noise injection radiometer

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Cited by 38 publications
(15 citation statements)
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“…In this mode, the radiometer is measuring the brightness temperature of a fixed region of the sky near the galactic pole to avoid influence from the Galactic emission. The known sky brightness temperature at L-band is then used to calibrate several MIRAS parameters such as antenna pattern errors, PMS gains and the reference radiometer coefficients [6].…”
Section: External Calibrationmentioning
confidence: 99%
“…In this mode, the radiometer is measuring the brightness temperature of a fixed region of the sky near the galactic pole to avoid influence from the Galactic emission. The known sky brightness temperature at L-band is then used to calibrate several MIRAS parameters such as antenna pattern errors, PMS gains and the reference radiometer coefficients [6].…”
Section: External Calibrationmentioning
confidence: 99%
“…The NIR consists of two independent receivers connected to a dual-polarization antenna and to an internal noise injection circuitry, so that all four Stokes parameters can be measured using the correlator matrix [4]. Its operation is based on an internal noise source which is used to balance the input signal to the receivers.…”
Section: Instrument Raw Datamentioning
confidence: 99%
“…However, in the NIR the so-called one-point calibration is applied. This means that the level of the noise injection is determined with one target, after which the antenna temperature can be determined using the physical temperature of the NIR and the ancillary data described in Section II [4]. In orbit, the space background radiation is foreseen to be used as the calibration target for NIR.…”
Section: Brightness Temperature In Antenna Reference Planesmentioning
confidence: 99%
“…A similar study was presented at IGARSS'04 [4] for the prototype of the NIR [5]. Novelty of this study, compared to the previous, lies on the facts that (1) it is based on more thorough temperature cycling, (2) it includes also the antenna and (3) the analysed model (EM) is representative to Flight Model of NIR.…”
Section: Introductionmentioning
confidence: 93%