VIA Technologies EPIA SN-Series Specifications Page 39

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FASTER
27
4.2 Proposed Solution
Before proceeding to the realization phase a list of requirements, arising from the
analysis of the state of the art technologies, was prepared and reported in the following
Table. Each requirement has been commented to clarify how it could be implemented in
the proposed solution.
Requirements
Comment
General Unit Requirements
RE.G.01
FASTER shall be designed to
be installed in a large variety
of ULA and GA airplanes
without any modifications to
the a/c structure and avionics.
Several adapter will be studied to make
the system compatible with different
aircrafts aerodynamic configuration.
For the purpose of this study only a
support plate for high wing aircrafts
will be developed.
Functional Requirements
RE.F.01
The system shall have the
capability to acquire high
resolution Earth images over a
large portion of the
electromagnetic spectrum
(ranging from visible to the
thermal infrared interval, 0.3
µm < λ < 14 µm)
In the FASTER system 2 colour CCD
cameras and a third camera equipped
with an nIR filter will be installed;
onboard free space will be left where a
microbolometer based TIR camera or a
compact SWIR camera added later.
RE.F.02
The system shall be able to
control and acquire more than
one sensing device using
different hardware interfaces
FASTER will use the GiGE Ethernet
interface as a standard high data rate
bus, USB will also be used to download
images while RS232, 422, 485 will be
available for camera timing and
parameters setting.
RE.F.03
Given the target area, the
system shall be able to
generate an appropriate
trajectory starting from the
departure aerodrome to last
selected waypoint
A planning tool will be developed to
rapidly generate flight trajectories given
departure and arrival airfield; the
planning tool is discussed in Chapter 5.
RE.F.04
The system shall be able to
guide the pilot through the
previously planned flight
A visual guidance interface has been
developed and presented in Section 6.6.
RE.F.05
The system shall be able to
acquire images of the selected
area only
Position information given by the GPS
receiver will be compared to the target
area coordinates and image acquisition
will be automatically started in order to
optimize data acquisition.
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