METimage is the Visible/Infrared Imaging mission (VII) on METOP-SG series, providing moderate resolution optical imaging of atmosphere and surface variables in multiple spectral channels ranging from 0.443 to 13.345 µm with a spatial sampling of 500 m. The instrument was developed by an industrial team led by Airbus Defense and Space GmbH on behalf of the German Space Administration Deutsches Zentrum für Luft und Raumfahrt (DLR) with funds from the German Federal Ministry of Transport and Digital Infrastructure and co-funded by EUMETSAT under DLR Contract No. 50EW1521. Hensoldt Optronics GmbH designed and manufactured two main components for the METimage instrument: the hyperspectral filter assemblies and the refractive relay infrared optics. The components are challenged by harsh environmental loads, while maximum optical performance must be met for precise data collection. Optics mounting was realized by sophisticated glue-free design, which had to be tested for long term sturdiness, stability and optical performance at cryo-vacuum conditions. Therefore, a well-tailored assembly and testing procedure was developed, based on an Optical Ground Support Equipment (OGSE) capable of illuminating and sensing wavefront errors at multiple MWIR and LWIR wavelength. After 6 years of development the project comes to an end and at the beginning of 2022 all flight models are delivered. Hensoldt Optronics GmbH shares in this paper insights into the testing strategies and setups for the relay optics. The design and functionality of the used OGSE is explained as also the importance of the accompanying optical modelling.
METimage will be the Visible/Infrared Imaging mission (VII) of the METOP-SG series. It is going to provide moderate ground resolution optical imaging of clouds, aerosols and surface variables in 20 spectral channels ranging from 443 to 13 345 nm with a spatial sampling of 500 m. The METimage instrument is in development by an industrial team led by Airbus Defence and Space GmbH on behalf of the German space administration DLR with funding from the German Federal Ministry of Transport and Digital Infrastructure (BMVI) and co funding by EUMETSAT under DLR Contract No. 50EW1521. In the context of this program Hensoldt Optronics GmbH designs, integrates and tests novel multispectral filter assemblies and refractive relay infrared optics for the METimage instrument. Both assemblies have to deliver optical performance in cryogenic-vacuum conditions post launch and deployment loads, which is a challenging demand. The development led to intricate glue-free mounting designs for filters and lenses. To establish the system’s optical performance a combination of prototyping, optical simulation, ambient adjustment and cryogenic-vacuum verification is necessary. For the latter a hexapod-carried OGSE was developed, capable to illuminate and sensing wavefront errors at multiple MWIR and LWIR wavelengths. This paper provides insights into the opto-mechanical designs of the relay optics and the hyperspectral filters. Furthermore the setups for adjustment and qualification tests will be described. The current project progress is reflected here within.
Recent satellites of the European Data Relay System (EDRS) are established with free-space optical (FSO) terminals. Operational FSO links in space are commercially available. Links between ALPHASAT or EDRS-A as GEO terminals and Sentinel LEO terminals are established with TRL 9. However laser links from the satellites through the atmosphere have a low Technical Readiness Level. Starting 2015 an Airborne Optical Communication (AOC) Demonstrator was developed by Hensoldt, which provides Air-to-Space unidirectional communication capabilities over approximately 40000 km distance (Geo orbit) at a data rate of 1.8 Gbit/s at a wavelength of 1064 nm with a laser power of approx. 15 W. The demonstrator was flown on an Airbus A310 aircraft. Successful links with user data streams from Tenerife to the GEO Alphasaat proved the function of AOC.
The typically used shortwave infrared spectral range (SWIR) between 900 nm and 1700 nm is a spectrally broader wavelengths range than the visible range. Available SWIR cameras generate a gray level image using the intensity over the entire spectral band. However, objects can exhibit completely different spectral behavior in this range. Plants have a high reflection at the lower end of the SWIR range and liquid water has a strong absorption band around 1400 nm, for example. We propose to divide the SWIR range into an appropriate number of spectral channels to extract more details from a captured image.
To extract this information the proposal follows a concept similar to color vision of the human eye. Analog to the three types of color receptors of the eye four spectral channels are defined for the SWIR. Each point of the image is attributed now by four “color values” instead of a single gray level.
For a comprehensive characterization of an object, a special SWIR colorimetry is possible by selecting appropriate filters with suitable band width and spectral overlap. The spectral sensitivity, the algorithms for calculating SWIR-color values, the discrimination of SWIR-color values by Noise Equivalent Wavelength Difference (NEWD) and spectral coded false color image display is discussed and first results with an existing SWIR camera are presented.
Current designs of combined VIS-color/SWIR camera optics use constant F-number over the full field of view (FOV)
range. Especially in the SWIR, limited space for the camera integration in existing system volumes and relatively high
pitch dimensions of 15μm or even 20μm force the use of relatively high F- numbers to accomplish narrow fields of view
less than 2.0° with reasonable resolution for long range observation and targeting applications. Constant F-number
designs are already reported and considered [1] for submarine applications. The comparison of electro-optical
performance was based on the given detector noise performance and sensitivity data by the detector manufacturer [1] and
further modelling of the imaging chain within linear MTF system theory.
The visible channel provides limited twilight capability at F/2.6 but in the SWIR the twilight capability is degraded due
to the relatively high F-number of F/7 or F/5.25 for 20 μm and 15 μm pitch, respectively. Differences between prediction
and experimental verification of sensitivity in terms of noise equivalent irradiance (NEI) and scenery based limiting
illumination levels are shown for the visible and the SWIR spectral range. Within this context, currently developed
improvements using optical zoom designs for the multispectral SWIR/VIS camera optics with continuously variable Fnumber
are discussed, offering increased low light level capabilities at wide and medium fields of view while still
enabling a NFOV < 2° with superior long range targeting capabilities under limited atmospherical sight conditions at
daytime.
Cameras for the SWIR wavelength range are becoming more and more important because of the better observation range for day-light operation under adverse weather conditions (haze, fog, rain). In order to choose the best suitable SWIR camera or to qualify a camera for a given application, characterization of the camera by means of the Minimum Resolvable Contrast MRC concept is favorable as the MRC comprises all relevant properties of the instrument. With the MRC known for a given camera device the achievable observation range can be calculated for every combination of target size, illumination level or weather conditions. MRC measurements in the SWIR wavelength band can be performed widely along the guidelines of the MRC measurements of a visual camera. Typically measurements are performed with a set of resolution targets (e.g. USAF 1951 target) manufactured with different contrast values from 50% down to less than 1%. For a given illumination level the achievable spatial resolution is then measured for each target. The resulting curve is showing the minimum contrast that is necessary to resolve the structure of a target as a function of spatial frequency. To perform MRC measurements for SWIR cameras at first the irradiation parameters have to be given in radiometric instead of photometric units which are limited in their use to the visible range. In order to do so, SWIR illumination levels for typical daylight and twilight conditions have to be defined. At second, a radiation source is necessary with appropriate emission in the SWIR range (e.g. incandescent lamp) and the irradiance has to be measured in W/m2 instead of Lux = Lumen/m2. At third, the contrast values of the targets have to be calibrated newly for the SWIR range because they typically differ from the values determined for the visual range. Measured MRC values of three cameras are compared to the specified performance data of the devices and the results of a multi-band in-house designed Vis-SWIR camera system are discussed.
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