Low Cost Inertial Navigation System
The developments, and the
performances improvement, of the Micro-Electro-Mechanical Systems (MEMS)
are rapidly changing the inertial sensors scenario. Their limited
volume, mass and power requirements, together with the low cost, make
them an interesting solution in the aerospace field.
Onboard balloons, where navigation
solution can be already provided by satellite navigation receivers, they
can efficiently offer a conservative back-up, but above all they would
provide attitude data and an increase of one order of magnitude in
available data rate.
A proposal for an inertial unit
intended to fly on balloons has been made by us, answering a ESA call
for student experiments onboard BEXUS balloon flights. The designed
navigation unit is based on three-gyros and three accelerometers,
calibrated with temperature sensors, packaged as a unique COTS part, and
includes a pressure sensor and a magnetometer for aiding. The navigation
solution will be compared with GPS-only mission data during the
post-proccessing.
The proposal succeeded and our
experiment flew onboard BEXUS 6, launched from Kiruna (Sweden) on 8th
October 2008 .
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