VIA Technologies EPIA SN-Series Specifications Page 13

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Introduction
1
Chapter 1. Introduction
Since 2003, the Microsatellite Laboratory of II Faculty of Engineering of the
University of Bologna has been involved in the design and realization of small satellite
missions based on the ALMASat multipurpose platform. After the realization of the first
microsatellite, ALMASat-1, it is currently under development a second Earth observation
mission, named ALMASat-EO. Goal of this second mission is the acquisition of mid-
resolution Earth images (in the visible band) of the Italian territory.
Besides the modification of the original ALMASat-1 bus, an entirely new optical
payload has to be assembled to achieve all mission requirements. The AMSC is a novel
concept of digital multispectral camera, based on the use of an LCD tunable filter instead
of a traditional filter wheel. This payload implies the use of new electronic architectures
that must ensure sufficient computational power to enable onboard image processing
(image compression and geographical tagging). Effect of all these new features is a longer
development phase and the need of specific tests necessary to reach an high reliability
level, compatible with typical space operations.
In order to perform both functional and radiometric tests, in an environment similar to
that in which the AMSC will operate, an aerial platform will be used. This solution, that
has several advantages, because of its complexity resulted in a completely independent
project, with more specific requirements compared to being just a test bed for ALMASat-
EO sensor.
FASTER stands for Fully Automated SysTem for Environmental monitoRing and this
acronym resumes the enhanced functionality given to the original test platform. The
project is jointly carried out together with the Flight Mechanics Laboratory of the II
Faculty of Engineering. Aim of the project is the realization of a compact, direct
georeferencing system capable to acquire very high resolution images in different bands
of the electromagnetic spectrum suitable to be mounted on very light aircraft platforms.
One of the most challenging objective to achieve is make a system which is independent
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