Testing of Airborne Laser Altimetry Sensors

This paper synthesizes the results of the mechanical shock, vibration and temperature tests that have been executed in order to verify the performance characteristics of the device under test (D UT) in environmental conditions representative of those which may be encountered during the operation of the equipment. In particular, the DUT is a laser sensor used for altimetry measurement on helicopter. The device will be mounted in the lower part of the aircraft.