PAGE CONTENTS
Objectives
Optical communication terminals (OCT) use laser beams to transfer data (e.g. Earth observation data) with high data rates from low-Earth orbit (LEO) satellites to geostationary satellites, which then forward the data to ground stations on Earth.
State-of-the-art optical communication systems are tailored for one-on-one communication links with one counter terminal at a time, over link sessions from a few minutes to hours. Link acquisition times in the order of tens of seconds are acceptable in these scenarios. When multiple simultaneous links or subsequent short duration links are required, this concept fails, as the acquisition time becomes significantly long compared to the link duration.
This is the case for ultra-high throughput satellites that implement multiple optical user access scenarios (e.g. constellations or airborne applications), as well as Galileo next-generation GNSS satellites. In addition, this is highly applicable to optical feeder links, as they require uninterrupted handover between multiple optical ground stations.
MUATS addresses the above described shortcoming of current optical link acquisition methods as well as acquisition and tracking sensors concepts for optical communication terminals (OCT).
Challenges
Optical communication terminals operate in NIR and SWIR wavelength ranges. For these wavelengths camera matrix detectors are rare and provide low resolutions (e.g. 640 x 512 pixels).
The first challenge is to find a detector for NIR and SWIR wavelengths that provide sufficient properties to achieve the required terminal position knowledge at the fully required field of view.
The required framerate of 200 Hz is the second challenge. The detector design has to provide the full frame readout capability of 200 Hz, which affects heavily the electronic architecture for this concept, in particular the FPGA and software performances.
The third challenge in the frame of this activity is the realization of a breadboard, which is able to demonstrate performance through measurement of representative simulated targets. This implies the determination and use of optimized algorithms for detection and tracking of the targets.
System Architecture
MUATS is designed as a single box and accommodates:
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2 identical, rad-hard refractive telescope optics
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2 InGaAs detectors with dedicated electronics
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and interleaved readout
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1 FPGA with dedicated electronics, including power supply and SpaceWire customer interface
The concept envisages that all necessary H/W is provided in one mechanical enclosure to enable autonomous operation and a simple redundancy concept. It considers the idea of interleaved detector readout regimes between two detectors, in order to reach a higher framerate with high resolution.
The MUATS concept study has furthermore provided a technical demonstrator (breadboard) based on commercial electronics and optics. The data processing has been realised with a standard PC.
Plan
The MUATS concept study started in April 2021 and ended in November 2022.
All activities have been completed, including:
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Definition of a technical baseline and creation of a detailed design
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Demonstration of functionalities and performance per simulations and analyses
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Implementation and development of a technical demonstrator (Breadboard), realization of a test campaign to demonstrate compliance to the technical requirements
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Assessment of the potential for commercial application and creation of a product development plan for raising TRL to qualification/flight model.
Current Status
The project is now completed.
