KEYWORDS: Diffusers, Bidirectional reflectance transmission function, Current controlled current source, Astronomical imaging, Simulation of CCA and DLA aggregates
This paper reports the result of an ESA study conducted at TNO to investigate properties of various diffusers. Diffusers are widely used in space instruments as part of the on-board absolute calibration. Knowledge of the behaviour of the diffuser is therefore most important.
From measurements of launched instruments in-orbit it has been discovered that when a diffuser is used in the vacuum of space the BRDF can change with respect to the one in ambient conditions. This is called the air/vacuum effect and has been simulated in this study by measuring the BRDF in a laboratory in ambient as well as vacuum conditions.
Another studied effect is related to the design parameters of the optical system and the scattering properties of the diffuser. The effect is called Spectral Features and is a noise like structure superimposed on the diffuser BRDF. Modern space spectrometers, which have high spectral resolution and/or a small field of view (high spatial resolution) are suffering from this effect. The choice of diffuser can be very critical with respect to the required absolute radiometric calibration of an instrument. Even if the Spectral Features are small it can influence the error budget of the retrieval algorithms for the level 2 products.
in this presentation diffuser trade-off results are presented and the Spectral Features model applied to the optical configuration of the MERIS instrument is compared to in-flight measurements of MERIS.
The paper provides an overview of the radiometric and spectral calibration of MERIS over its 10 years of operations. An overview of the instrwnent, of the radiometric and spectral calibration principles and an outline of the calibration processing chain are presented.
The paper describes the change in methodology for the determination of the long term radiometric trending (gain
degradation) used in the 3rd MERIS mission reprocessing. An overview of the instrument, the principles of its
radiometric calibration and an outline of the calibration processing chain are presented, a review of the trending
approach taken for the 2nd MERIS mission reprocessing is provided and its limitations shown. The results from the more
robust trending approach taken for the 3rd MERIS reprocessing are provided and compared to these of the 2nd MERIS
reprocessing.
The paper intends to describe the operational processing of the MERIS Radiometric Calibration. An overview of the
instrument, the principles of its radiometric calibration and an outline of the calibration processing chain are presented.
The various models used within the calibration processing are described and discussed. A status of the error budgets and
uncertainties of on-ground and in-flight measurements, of models performances, and finally of the expected radiometric
accuracy is given.
This paper reports the activities performed in the framework of the ESA contract 18432/04/NL/AR: Enhancement of diffusers BSDF Accuracy.
This study was conducted to investigate properties of various diffusers. Diffusers are widely used in space instruments as part of the on-board absolute calibration. Knowledge of the behavior of the diffuser is therefore most important.
From measurements of launched instruments in-orbit it has been discovered that when a diffuser is used in the vacuum of space the BSDF (Bi-directional Scattering Distribution Function) can change with respect to the one in ambient conditions. This is called the air/vacuum effect and has been simulated in this study by measuring the BSDF in a laboratory in ambient as well as vacuum conditions, results of this part of the study will be reported.
Another effect on the BSDF is not related to the air/vacuum effect, but to the design parameters of the optical system and the scattering properties of the diffuser. The effect is called Spectral Features and is a noise like structure superimposed on the BSDF. To observe this effect, spectral and spatial (partially) coherence light is needed. High-resolution spectrometers provide the spectral coherence and a narrow field of view provides the spatial coherence. Modern space spectrometers have high spectral resolution and/or a small field of view (high spatial resolution).
Different diffusers create different speckle patterns leading to different Spectral Features amplitudes. Therefore the choice of diffuser can be very critical with respect to the required absolute radiometric calibration of an instrument. Even if the Spectral Features are small it can influence the error budget of the retrieval algorithms for the level 2 products.
In this presentation diffuser trade-off results are presented and the Spectral Features model applied to the optical configuration of the MERIS instrument is compared to in-flight measurements of MERIS.
The introduction describes the use of diffusers in earth-observation satellites and why they cause spectral features. In Sec.2 the physical background of the spectral features, speckles, is discussed. Section 3 shows the results from air/vacuum effect measurements (SubSec.3.1), spectral features amplitude measurements on our in-house setup and simulations in a single graphical display (SubSec.3.2 ), and the measured and simulated results for the MERIS instrument (SubSec.3.3). The following sections deal with a description of the measuring setup and the model that has been made to do the simulations. Finally, in the discussion, topics like what is the best diffuser and what can be done to minimize the amplitude of the spectral features will be dealt with.
Envisat is ESA's environmental research satellite launched on 1 March 2002. It carries a suit of sensors offering opportunities for a broad range of scientific research and applications.
The radiometric calibration results from the first 2 years of operation of the MEdium Resolution Imaging Spectrometer (MERIS) will be presented. Radiometric calibration using the on-board diffuser will be discussed and compared with the results from a number of vicarious calibration methods and the image quality of instrument will be assessed.
Since the launch of MERIS on ENVISAT long term activities using vicarious calibration approaches are set in place to monitor potential drifts in calibration in the radiance products of MERIS. We are using a stable, well monitored reference calibration site (Railroad Valley, Nevada, USA) to derive calibration uncertainties of MERIS over time. We are using interpolation of uncertainties to derive a second set of uncertainties for a national data validation in the Netherlands. A satellite image derived land use map of the Netherlands (LGN4) is used to determine the largest homogeneous land use classes using a standard purity index (SPI). Potential adjacency effects are minimized using moving window filters on the pixels of the aggregated map. Multiple error propagation is being used to assess the impact of calibration accuracy on land use classification. A classification in 9 land use classes is finally performed on MERIS FR images of the Netherlands using image based spectral unmixing and matched filtering with endmembers derived from the LGN. We conclude that the classification performance may significantly be increased, when taking into account long-term vicarious calibration results.
Envisat is ESA's environmental research satellite launched on 1 March 2002. It carries a suit of sensors offering opportunities for a broad range of scientific research and applications.
The spectral calibration results from the first 2 years of operation of the MEdium Resolution Imaging Spectrometer (MERIS) will be presented. Four different methods, Making use of the spectral programmability of the instrument, were used to characterize the five MERIS spectrometers at eight wavelengths covering most of the useful spectral range of the instrument.
The onboard spectral calibration uses an Erbium doped SpectralonTM diffuser panel providing useful absorption features at 408 & 522 nm. Configuring the instrument band settings to cover a designated spectral ranges with narrow bands, and acquiring data over natural targets for a limited number of orbits, as well as using the on-board radiometric (white) SpectralonTM diffuser; the instrument's response to a number of Fraunhofer absorption features {395, 486, 656, 854 & 866 nm}, and atmospheric oxygen absorption {760nm} where analysed. The methods and results of this analysis will be presented as well as the final MERIS spectral model derived from these.
Envisat is ESA's environmental research satellite launched on 1 March 2002. It carries a suit of sensors offering opportunities for a broad range of scientific research and applications. The calibration results from the first year of operation of the MEdium Resolution Imaging Spectrometer (MERIS) will be presented, including in-flight verification and radiometric, spectral and geometric characterization of the instrument. Radiometric calibration using the on-board diffuser will be discussed and comparison with vicarious calibration results over desert sites or well-characterized marine sites will be presented. The image quality will be assessed, and improvements resulting from the in-flight characterization will be presented.
ENVISAT, ESA's ENVironmental research SATellite, has been launched successfully on 1 March 1st 2002. On-board, MEdium Resolution Imaging Spectrometer MERIS, is responding nominally. The results from the first six-months of in-flight verification and characterization of the instrument will be presented. The evolution of the instrument radiometric response based on the radiometric calibration results using the on-board diffusers will be discussed. The results from dedicated spectral characterization campaigns based on the spectral features of the sun (Fraunhofer), atmospheric oxygen and Erbium (doped diffuser) will be presented, and the instrument's spectral model derived will be discussed.
The Medium Resolution Imaging Spectrometer (MERIS), developed by the European Space Agency (ESA) for the Envisat polar orbit Earth mission, belongs to a new generation of ocean colour sensors which will yield a major improvement in the knowledge of such a crucial processes as the ocean contribution to the carbon cycle. The global mission of MERIS will have a major contribution to scientific projects which seek to understand the role of oceans and ocean productivity in the climate system and our ability to forecast change through models. Secondary objectives of the MERIS mission will be directed to the measurement of atmospheric parameters associated with clouds, water vapour and aerosols in addition to land surface parameters, important in particular for the understanding of vegetation processes. MERIS measures the radiance reflected from the Earth's surface in the visible and near infra-red part of the spectrum. Data are transmitted in fifteen spectral bands of programmable width and location. The instrument features two spatial resolution and several observation and calibration modes selectable by ground command. This paper gives an overview ofthe instrument mission, its concept and data products.
The medium imaging spectrometer (MERIS), developed by the European Space Agency (ESA) for the ENVISAT-1 polar orbit Earth mission, belongs to a new generation of ocean color sensors which will yield a major improvement in the knowledge of such a crucial processes as the ocean contribution to the carbon cycle. MERIS measures the radiance reflected from the Earth's surface in the visible and near infrared part of the spectrum. Data are transmitted in fifteen spectral bands of programmable width and location. The instrument features tow spatial resolution and several observation and calibration modes selectable by ground command. The instrument development is currently carried out by an international team led by AEROSPATIALE under ENVISAT prime contractor ship of DORNIER. The development of the instrument has now reached a status where the instrument has been proven to be compliant with the scientific requirements. This paper gives an overview of the instrument, its design with emphasis given to the acquisition and on-board processing chains. A summary of the major performance sand interface budgets is also provided.
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