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AIMMS-20 probes are permanentely installed on both aircrafts. Removal of the probes from the aircraft and re-installation requires calibration flight maneuvers and recalculation of the calibration coefficients.

Summary

The AIMMS (Aircraft Integrated Meteorological Measurement System) is a fully-integrated instrumentation system providing high-accuracy measurements of temperature, telative humidity, three-dimensional winds and turbulence. The embedded GPS / Inertial subsystem also provides measurement of inertial accelerations (X, Y, Z), inertial angular rates (P, Q, R), GPS time, position and velocity as well as attitude (roll, pitch, yaw).

Manufacturer Aventech Research Inc.
Model AIMMS-20
Serial No. n/a
Type airspeed vector system
REGISTRY-Link ↪ REGISTRY (6804)

Contacts

Name Institution Role
Martin Gehrmann Alfred Wegener Institute, Helmholtz Centre for Polar and Marine Research Device Contact

Available Devices and Specifications

Despite the air data probe installed under the wing, the AIMMS20 system comprises 4 AIMMS-20 modules (GPS, IMU, Digital I/O and CMP) which are permanently  installed in the underfloor compartment. An additional I/O module is installed in a rack for data storage during flight.

Name Model Serial Number REGISTRY-Link
Aircraft Integrated Meteorological Measurement System AIMMS-20 ADP121103 ↪ REGISTRY (6805)
Aircraft Integrated Meteorological Measurement System AIMMS-20 ADP030802 ↪ REGISTRY (6806)

Specifications of the air data probe AIMMS20

Specifications of an AIMMS20 module

Position

InfoThe AIMMS-20 is permanently installed under the right wing of the aircraft.
X0.0 none
(no description given)
Y0.0 none
(no description given)
Z0.0 none
(no description given)

Data logging, storage and archiving

Logged parameter

Parameter O2ARegistry Output Type Unit
relative humidity relative humidity none
barometric pressure barometric pressure Pa
wind flow vector north component speed m/s
wind flow vector east component speed m/s
latitude latitude deg
longitude longitude deg
altitude altitude m
north probe velocity speed m/s
east probe velocity speed m/s
down probe velocity speed m/s
bank angle angular rates deg
pitch angle angular rates deg
heading angle angular rates deg
true airspeed speed m/s
vertical wind speed m/s
sideslip angle angular rates deg
angle of attack angular rates none
sideslip signal angular rates none

Rawdata storage on board

Data archiving on land

Documentation

Also see https://sensor.awi.de/ for calibration certificates of the sensors.


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