Lens R&D and SystematIC Design B.V. are currently involved, in frame of an Artes AT program, in designing a small true digital Sunsensor, intended to have an as large as possible Field Of View (FOV). Adding another 10 degrees to the common 60° on axis field of view will even provide a redundant full spherical coverage with only 8 sensors, (instead of the required 10 sensors when a sensor with 60° FOV is used). This conclusion prompted an investigation into the possibilities to increase the FOV to 69° on axis. During the following design considerations however, several optical issues were encountered, actually leading to a proposal to reduce the FOV to 62° in diagonal (54° on axis). This paper focusses on these issues and effects, like polarisation dependent reflection, Sun spot spreading and shadowing effects of on-chip interconnects.
For many years there have been attempts to eliminate the earth albedo sensitivity for Sunsensors. This is best done through development of a true digital Sunsensor.
The best known digital Sunsensor was designed (and patented) by Adcole back in the 1970's only to be followed by the Leonardo smart digital Sunsensor and a small digital Sunsensor developed by Sinclair interplanetary some 30 years later. The first two sensors are relatively large and expensive, whereas the later is small and affordable but lacks the required radiation tolerance and quality level required for longer duration ESA missions. Although TNO attempted to develop a small but highly reliable Sunsensor between 2004 and 2010, this development did not lead further than the prototype called mini-DSS.
From this TNO research and developments it became apparent that the detector technology and detection principle used are key to delivering the desired properties: high reliability, low cost, small form factor and low power consumption.
While Leonardo stopped the development of a small digital Sunsensor in 2017, Lens R&D is now developing such a device in frame of an ESA Artes 5.1 contract signed in April 2018.
Based on insights developed during the TNO mini/micro-DSS program and a new operating principle, the Intensity Based Images Sensing (IBIS) principle is expected to lead to a producible sensor that is low power, highly reliable and cost effective.
The dedicated imager (dubbed IPS) required for the demonstrator to be built within the framework will be designed by SystematIC Design and is expected to show a very low power consumption and low operation voltage. These properties are important in order to allow for further design optimizations related to potential autonomous powering or power over data applications.
The presentation will focus on the status of the Artes program design considerations for the IBIS sensor and the optical design of the sensor, which is core to providing a highly reliable but cost-effective sensor.
Optimum application of micro system technologies allows building small sensor systems that will alter procurement strategies for spacecraft manufacturers. One example is the decreased size and cost for state of the art sunsensors. Integrated sensor systems are being designed which, through use of microsystem technology, are an order of magnitutde smaller than most current sunsensors and which hold due to the large reproducibility through batch manufacturing the promise of drastic price reduction. If the Commercial Of The Shelf (COTS) approach is adopted by satellite manufacturers, this will drastically decrease mass and cost budgets associated with sunsensing applications.
Ongoing miniaturization of spacecraft demands the reduction in size of Attitude and Orbit Control Systems (AOCS). Therefore TNO has created a new design of a multi aperture, high performance, and miniaturized star tracker. The innovative design incorporates the latest developments in camera technology, attitude calculation and mechanical design into a system with 5 arc seconds accuracy, making the system usable for many applications. In this paper the results are presented of the system design and analysis, as well as the performance predictions for the Multi Aperture Baffled Star Tracker (MABS). The highly integrated system consists of multiple apertures without the need for external baffles, resulting in major advantages in mass, volume, alignment with the spacecraft and relative aperture stability. In the analysis part of this paper, the thermal and mechanical stability are discussed. In the final part the simulation results will be described that have lead to the predicted accuracy of the star tracker system and a peek into the future of attitude sensors is given.
Current Thermal infra red ( 7..14μm) multispectral imager instruments use cryogenically cooled Mercury Cadmium Telluride (MCT or HgCdTe) detectors. This causes the instruments to be bulky, power hungry and expensive.
For systems that have medium NETD (Noise Equivalent Temperature Difference) requirements and can operate with high speed optics (<1.5), room temperature microbolometer performance has increased enough to enable people to design multispectral instruments based on this new detector technology.
Because microbolometer technology has been driven by the military need for inexpensive, reliable and small thermal imagers, microbolometer based detectors are almost exclusively available in 2D format, and performance is still increasing.
Building a spectrometer for the 7 to 12 μm wavelength region using microbolometers has been discarded until now, based on the expected NETD performance.
By optimising the throughput of the optical system, and using the latest improvements in detector performance, TNO TPD has been able to design a spectrometer that is able to provide co-registered measurements in the 7 to 12 μm wavelength region yielding acceptable NETD performance.
Apart from the usual multispectral imaging, the concept can be used for several other applications, among which imaging in both the 3 to 5 and 7 to 12 μm atmospheric windows at the same time (forest fire detection and military recognisance) or wideband flame analysis (Nox detection in industrial ovens).
MIBS is a spectrometer operating in the thermal infrared wavelength region, designed in frame of the phase A study for the ESA EarthCARE mission as part of the multispectral Imaging instrument MSI, which uses a 2D microbolometer array detector in stead of the more common MCT detectors.
Utilization of a microbolometer and using an integrated calibration system, results in a sensor with a size and mass reduction of at least an order of magnitude when compared to currently flying instruments with similar spectral resolution.
In order to demonstrate feasiblity a breadboard has been designed, which will be build and aligned in 2006 and will be ready for testing the forth quarter of 2006.
Applying freeform optics in high-end optical systems can improve system performance while decreasing the system mass, size and number of required components. Their widespread application is however held back by the lack of a suitable metrology method. TNO, TU/e and NMi VSL have therefore developed the NANOMEFOS measurement machine [1], capable of universal non-contact and fast measurement of aspherical and freeform optics ranging from convex to concave and from flat to freeform, up to ⊘500 mm, with an uncertainty below 30 nm (2σ).
What started as an academic development in frame of the Dutch MicroNed program five years ago should culminate in the introduction of the smallest digital sunsensor available in (and probably outside) of Europe at the ICSO. At the ICSO, TNO plans to show for the first time a working mini-DSS, based on the APS+ chip. The sunsensor has been optimized for low power, low recurring costs and high repeatability in production. In order to achieve this, several innovations have been included and verified in a diverse range of supporting programs. During the presentation, trades performed that lead to the current setup, as well as the properties of the sensor system and interfaces will be discussed.
Johan Leijtens, Willem Vliegenthart, Dimitris Lampridis, Giuseppe Vacanti, Bert Monna, Elbert Bechthum, Koen Hagenaars, Erik van der Heide, Michiel Kruijff, Eddie van Breukelen, Anita LeMair
In the frame of the Dutch Prequalification for ESA Programs(PEP), as part of the efforts to design an integrated optical attitude control subsytem (IOPACS), a consortium of TNO and several SME's in the Netherlands have been working on a novel type of startracker called MABS (Multiple Aperture Baffled Startracker). The system comprises a single cast metal housing with four reflective optical telescopes which use only structural internal baffling. Inherent to the design are a very high stability and excellent co-alignment between the apertures, a significant decrease in system size and low recurring production cost. The concept is a radical change from more common multiple startracker setups. The presentation will concentrate on the validity of the concept, the predicted performance and benefits for space applications, the produced breadboard and measured performances as well as the costing aspects.
Lens R&D is currently working on an Artes 5-2 contract aimed at developing an ITAR free extended temperature sunsensor. This sensor should be able to survive the temperature excursions associated with mounting on an extendable solar panel of geostationary satellites.
The microbolometer spectrometer breadboard MIBS is a prism spectrometer that uses an uncooled microbolometer
detector array and has been designed for the ESA EarthCARE mission. In order to demonstrate its feasibility a
breadboard has been build, and tests have been performed that show good correlation between predicted and achieved
results. Although application for EarthCARE has become uncertain due to geodistribution issues, it is feld that this
instrument (which is small enough to give grown up performance to a micro satellite) has a lot of application potential
for applications like weather forecasting and forest fire detection. The presentation will elaborate on performance
predicted, measurements performed, results achieved and future applications.
It is generally known that active pixel sensors (APS) have a number of advantages over CCD detectors if it comes to cost
for mass production, power consumption and ease of integration. Nevertheless, most space applications still use CCD
detectors because they tend to give better performance and have a successful heritage. To this respect a change may be at
hand with the advent of deep sub-micron processed APS imagers (< 0.25-micron feature size). Measurements performed
on test structures at the University of Delft have shown that the imagers are very radiation tolerant even if made in a
standard process without the use of special design rules. Furthermore it was shown that the 1/f noise associated with deep
sub-micron imagers is reduced as compared to previous generations APS imagers due to the improved quality of the gate
oxides. Considering that end of life performance will have to be guaranteed, limited budget for adding shielding metal
will be available for most applications and lower power operations is always seen as a positive characteristic in space
applications, deep sub-micron APS imagers seem to have a number of advantages over CCD's that will probably cause
them to replace CCD's in those applications where radiation tolerance and low power operation are important
CMOS APS technology allows including signal processing in the sensor array. Inclusion of functionality however will
come at a cost both financially and in the field of limited applicability. Based on two real world examples (micro digital
sunsensor core and lightning flash detector for Meteosat Third Generation (MTG)) it will be demonstrated that large
system gains can be obtained by devising smart focal planes. Therefore it is felt that the advantages outweigh the
disadvantages for some applications, making it worth to spend the effort on system integration.
KEYWORDS: Satellites, Sensors, Space operations, Signal to noise ratio, Electronics, Aerospace engineering, Telescopes, Solar cells, Optical components, Space telescopes
Micro systems technology allows building ever-smaller systems. This has lead to many activities all over the world that
are focused on building micro- and nano satellites. Most of these satellites are seen as technology qualifiers, meaning
that they are used to prove that the developed technology can be used on board of spacecraft and can survive the launch
environment. At this moment in time there is so much technology available and under development that one can start to
think about building mature satellites on a micro scale (mature in the sense that the satellite can perform a scientifically
or socially significant function). For satellites with an optical payload, a minimum aperture and baffle size are required,
thus setting a minimum size for the satellite. The overall size of the satellite can be reduced by building the satellite
around the instrument instead of building an instrument that is put on top of a satellite bus.
MIBS is a spectrometer operating in the thermal infrared wavelength region, designed in frame of the phase A study for the ESA EarthCARE mission as part of the multispectral Imaging instrument MSI, which uses a 2D microbolometer array detector in stead of the more common MCT detectors.
Utilization of a microbolometer and using an integrated calibration system, results in a sensor with a size and mass reduction of at least an order of magnitude when compared to currently flying instruments with similar spectral resolution.
In order to demonstrate feasibility a breadboard has been designed, which will be build and aligned in 2006 and will be ready for testing the forth quarter of 2006.
With the advent of interplanetary missions, requirements posed on satellite instrumentation are becoming increasingly difficult to meet. The main problems are associated with the very limited mass and volume budgets in combination with extreme temperatures and radiation environment. All of the new requirements will have to be met without loosing the prime instrument or sensor performance. This requires a fundamentally different approach. Through the use of Microsystems engineering in combination with clever design both volume and mass can be decreased by more than an order of magnitude while drastically increasing ruggedness. In the end this approach may lead to a paradigm shift in the sense that very capable and rugged sensors will be procure also for more benign missions due to the cost advantages of using MST. The paper will focus on application of MST technologies for sunsensors generally used in the Attitude and orbit control subsystem of satellites and the possible gains (both technological and application wise).
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