The NASA GSFC Filter Radiometer Monitoring System (FRMS) was used to compare lamp-based and detector-based spectral radiance calibration of an integrating sphere. The FRMS is a telecentric, filter radiometer employing two apertures, a filter wheel, and a detector. The FRMS uses nine filters at specific wavelengths from 360 to 2400 nm. The lamp-based calibration used a National Institute of Standards and Technology (NIST) calibrated irradiance standard lamp to calibrate the irradiance responsivity of a scanning spectroradiometer. The spectroradiometer was then used to transfer its irradiance calibration to an integrating sphere. The lamp-based spectral radiance calibration of the sphere was calculated using the sphere irradiance, the sizes of the sphere exit and spectroradiometer entrance apertures, and the distance between those apertures. The detector-based calibration of the sphere used NIST calibrated absolute radiance Si photodiode detector to determine the absolute spectral radiance responsivity of the FRMS with the NASA GSFC Automated Laser Tuned Advanced Radiometry (ALTAR) laser system as the source. The absolute spectral radiance responsivity of the FRMS was measured at the following channels: 380, 410, 640, and 840, nm. The FRMS measured the integrating sphere to make a direct determination of its absolute radiance at those channels. Analysis of lamp-based and detector-based radiance measurements of the integrating sphere at four wavelength bands will be presented.
A KHz Pulsed Laser Detection System was developed employing the concept of charge integration with an electrometer, in the NASA Goddard Space Flight Center, Code 618 Calibration Lab for the purpose of using the pulsed lasers for radiometric calibration. Comparing with traditional trans-impedance (current-voltage conversion) detection systems, the prototype of this system consists of a UV-Enhanced Si detector head, a computer controlled shutter system and a synchronized electrometer. The preliminary characterization work employs light sources running in either CW or pulsed mode. We believe this system is able to overcome the saturation issue when a traditional trans-impedance detection system is used with the pulsed laser light source, especially with high peak-power pulsed lasers operating at kilohertz repetition rates (e.g. Ekspla laser or KHz OPO). The charge integration mechanism is also expected to improve the stability of measurements for a pulsed laser light source overcoming the issue of peak-to-peak stability. We will present the system characterizations including signal-to-noise ratio and uncertainty analysis and compare results against traditional trans-impedance detection systems.
A Light-Emitting Diode (LED)-driven integrating sphere light source has been fabricated and assembled in the NASA Goddard Space Flight Center (GSFC) Code 618 Biospheric Sciences Laboratory’s Calibration Facility. This light source is a 30.5 cm diameter integrating sphere lined with Spectralon. A set of four LEDs of different wavelengths are mounted on the integrating sphere’s wall ports. A National Institute of Standards and Technology (NIST) characterized Si detector is mounted on a port to provide real-time monitoring data for reference. The measurement results presented here include the short-term and long-term stability and polarization characterization of the output from this LED-driven integrating sphere light source. As an initial application, this light source is used to characterize detector/pre-amplifier gain linearity in light detection systems. The measurement results will be presented and discussed.
A tunable, intensity-stabilized, quasi-continuous wave (CW) laser system, patterned after the Spectral Irradiance and Radiance Responsivity Calibrations using Uniform Sources (SIRCUS) system at the National Institute of Standards and Technology (NIST) 1, has been installed and is being tested in the NASA Goddard Space Flight Center (GSFC) Code 618 Biospheric Sciences Laboratory’s Calibration Facility. This system is referred to as SIRCUS-G (SIRCUS-Goddard). The tunable output of the laser system is fiber-fed to a 76.2 cm diameter integrating sphere lined with Spectralon. The uniform radiance light emitted from the integrating sphere is used in system-level radiometric responsivity characterizations and wavelength calibrations of remote sensing instruments. The primary radiance reference standards in the responsivity characterizations are a three-element Si trap radiometer for the visible and near infrared and a radiometer employing an InGaAs detector. Both radiometers have been calibrated by NIST. These radiometers are located at the exit port of the Spectralon coated integrating sphere. In addition, a set of three radiometers are mounted on the 76.2 cm integrating sphere’s wall ports to monitor source radiance and to provide real-time sphere radiance data during the calibrations of remote sensing instruments. These monitor radiometers provide spectral coverage from 300nm to near 2500nm. This paper presents the results of our characterization of the performance of these monitor radiometers. Results are presented and discussed on monitor radiometer short- and long-term system stability, noise level, and total measurement uncertainty.
The NASA Goddard Space Flight Center (GSFC) Radiometric Calibration Laboratory (RCL) maintains several large integrating sphere sources covering the visible to the shortwave infrared wavelength range. Two critical, functional requirements of an integrating sphere source are short- and long-term operational stability and repeatability. Monitoring the source is essential in determining the origin of systemic errors, thus increasing confidence in source performance and quantifying repeatability. If monitor data falls outside the established parameters, this could be an indication that the source requires maintenance or recalibration against the National Institute of Science and Technology irradiance standard. The GSFC RCL has developed a Filter Radiometer Monitoring System (FRMS) to continuously monitor the performance of its integrating sphere calibration sources in the 400 to 2400 nm region. Sphere output change mechanisms include lamp aging, coating (e.g., BaSO4) deterioration, and ambient water vapor level. The FRMS wavelength bands are selected to quantify changes caused by these mechanisms. The FRMS design and operation are presented, as well as data from monitoring four of the RCL's integrating sphere sources.
Optical spectroradiometers used to measure and monitor the radiance output of uniform sources must be thoroughly
characterized. The viability of the use of an instrument for such purposes is based upon the establishment of knowledge
of its radiometric responsivity characteristics. The NASA Goddard Space Flight Center Radiometric Calibration
Laboratory (RCL) has commissioned a new spectroradiometer for use in measurements of irradiance and radiance
sources. The spectroradiometer is comprised of a commercial scanning grating, Czerny-Turner double monochromator.
This spectroradiometer has been used to make measurements on a number of irradiance and radiance sources over the
wavelength range of 300 to 2400 nm. Instrument characterization included determination of stability, functional
wavelength calibration and scattered light performance. Comparison measurements were also made with other
radiometers. The data gathered from these measurements is presented, analyzed, and discussed.
The NASA Goddard Space Flight Center (GSFC) Radiation Calibration Facility (RCF) maintains several large
integrating sphere sources covering the visible and near infrared wavelength range. Two critical requirements of an
integrating sphere source are short and long-term operational stability and repeatability. Monitoring the source is
essential in determining the origin of systemic errors, thus increasing confidence in source performance, and quantifying
repeatability. If monitor data falls outside the established parameters, this is an indication that the source requires
maintenance or re-calibration against the National Institute of Science and Technology (NIST) irradiance standard. The
GSFC RCF has developed a Filter Radiometer Monitoring System (FRMS) to continuously monitor the performance of
its integrating sphere calibration sources in the 400-2400nm region. Sphere output change mechanisms include lamp
aging, coating (BaSO4) deterioration, and ambient water vapor level. The FRMS wavelength bands are selected to
quantify changes caused by these mechanisms. The FRMS design and operation is presented, as well as data from
monitoring three of the RCF's integrating sphere sources.
In June 2007, a spherical integrating source was calibrated in the National Aeronautics and Space Administration
(NASA) Goddard Space Flight Center's (GSFC) Calibration Facility as part of the prelaunch characterization program
for the NPOESS Preparatory Program (NPP) Ozone Mapping and Profiler Suite (OMPS) instrument. Before shipment to
the instrument vendor, the sphere radiance was measured at the Remote Sensing Laboratory at the National Institute of
Standards (NIST) and then returned to the NASA Goddard facility for a second calibration. For the NASA GSFC calibration,
the reference was a set of quartz halogen lamps procured from NIST. For the measurement in the Remote
Sensing Laboratory, the reference was an integrating sphere that was directly calibrated at NIST's Facility for Spectroradiometric
Calibrations (FASCAL). For radiances in the visible and near-infrared (400 nm to 1000 nm), the agreement
between the NASA GSFC calibration and the validation measurements at the Remote Sensing Laboratory was at the 1 %
level. For radiances in the near ultraviolet (250 nm to 400 nm), the agreement was at the 3 % level.
As part of an effort to reduce uncertainties in the radiometric calibrations of integrating sphere sources and standard lamp irradiance sources, the Goddard Space Flight Center (GSFC) Radiometric Calibration Facility's (RCF) primary radiometer was characterized at the NIST facility for Spectral Irradiance and Radiance Calibrations with Uniform Sources (SIRCUS). Based on those measurements, a nominal slit scattering function was developed for the radiometer. This allowed calculations of band averaged spectral radiances and irradiances for the radiometer's measurements of sphere and standard lamp sources, respectively. From these calculations the effects of bandwidth and spectral stray light were isolated for measurements in the blue spectral region. These effects, which depend on the spectral distribution of the source being measured, can be as large as 8% for measurements at 400 nm. The characterization results and a correction algorithm for these effects are presented here.
As part of an effort to reduce uncertainties in the radiometric calibrations of integrating sphere sources and standard lamp irradiance sources, the Goddard Space Flight Center (GSFC) Radiometric Calibration Facility (RCF) primary radiometer was characterized at the NIST facility for Spectral Irradiance and Radiance Calibrations with Uniform Sources (SIRCUS). Specifically, the radiometer's slit spectral function was measured and the magnitude of out-of-band stray light was determined. The characterization also revealed significant contributions of spectral stray light due to fluorescence of the radiometer's input sphere. The RCF examined the effects of stray light and sphere fluorescence in the radiometer on source radiance calibrations along with approaches to reduce those sources of measurement error.
For over three decades, the Radiometric Calibration Facility (RCF) at NASA's Goddard Space Flight Center (GSFC) has maintained calibrated uniform radiance sources for use by the global remote sensing community. As part of a continuing effort to reduce measurement uncertainties while improving efficiency, the calibration transfer hardware and operational protocols are systematically examined, with improved equipment and techniques being incorporated. This paper describes the optical characterization and presents radiance measurements of a new spectroradiometer, the GSFC 750/Integrating Sphere Irradiance Collector (ISIC), using a new input optical system. The performance of the new input optical system is compared with the two previous input systems.
Two critical requirements of any calibration source are short and long-term operational stability and repeatability. Source monitoring is necessary in quantifying overall source performance including stability and repeatability. The NASA GSFC Code 920.1 Radiance Calibration Facility (RCF) developed a Filter Radiometer Monitoring System (FRMS) to continuously monitor the performance of its integrating sphere calibration sources. FRMS bands are in the 0.4 -2.4 μm region, with several bands selected to coincide with common remote sensing bands. The FRMS was designed and fabricated in the year 2000. Early in 2001, the FRMS was reconfigured prior to being deployed on the RCF 180cm integrating sphere. This paper describes the instrument modifications resulting from the FRMS reconfiguration and presents FRMS monitor data for three RCF integrating sphere sources.
Two critical requirements of a calibration source are short- and long-term operational stability and repeatability. Monitoring the source is an asset in determining the origin of temporal changes, thus increasing confidence in source performance and quantifying repeatability. Monitor data which fall outside established parameters indicate that the source requires maintenance or re-calibration against the standard. The NASA GSFC Code 920. 1 Radiance Calibration Facility (RCF) has developed a Filter Radiometer Monitoring System (FRMS) to continuously monitor the performance of its integrating sphere calibration sources in the 400-2400nm region. Sphere output change mechanisms include lamp aging, coating (BaSO4) deterioration, and water vapor level. FRMS wavelength bands are selected to be sensitive to changes caused by these mechanisms. Several FRMS bands coincide with common remote sensing instrument bands.
EOS satellite instruments operating in the visible through the shortwave infrared wavelength regions (from 0.4 micrometer to 2.5 micrometer) are calibrated prior to flight for radiance response using integrating spheres at a number of instrument builder facilities. The traceability of the radiance produced by these spheres with respect to international standards is the responsibility of the instrument builder, and different calibration techniques are employed by those builders. The National Aeronautics and Space Administration's (NASA's) Earth Observing System (EOS) Project Science Office, realizing the importance of preflight calibration and cross-calibration, has sponsored a number of radiometric measurement comparisons, the main purpose of which is to validate the radiometric scale assigned to the integrating spheres by the instrument builders. This paper describes the radiometric measurement comparisons, the use of stable transfer radiometers to perform the measurements, and the measurement approaches and protocols used to validate integrating sphere radiances. Stable transfer radiometers from the National Institute of Standards and Technology, the University of Arizona Optical Sciences Center Remote Sensing Group, NASA's Goddard Space Flight Center, and the National Research Laboratory of Metrology in Japan, have participated in these comparisons. The approaches used in the comparisons include the measurement of multiple integrating sphere lamp levels, repeat measurements of select lamp levels, the use of the stable radiometers as external sphere monitors, and the rapid reporting of measurement results. Results from several comparisons are presented. The absolute radiometric calibration standard uncertainties required by the EOS satellite instruments are typically in the plus or minus 3% to plus or minus 5% range. Preliminary results reported during eleven radiometric measurement comparisons held between February 1995 and May 1998 have shown the radiance of integrating spheres agreed to within plus or minus 2.5% from the average at blue wavelengths and to within plus or minus 1.7% from the average at red and near infrared wavelengths. This level of agreement lends confidence in the use of the transfer radiometers in validating the radiance scales assigned by EOS instrument calibration facilities to their integrating sphere sources.
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