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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).

aircraft:bt-67:aimms20 (6804)


$body No images available.

Contacts

No contacts available.

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. No subdevices available.

Specifications of the air data probe AIMMS20

Dimension (diameter x L)

38 - 76 mm x 620 mm, max. width 188 mm, pylon height 229mm

Weight

23.4 kg

Power Supply

28 VDC

Data interface

CAN Bus, RS-232, USB via I/O module

Specifications of an AIMMS20 module

Dimension (L x W x H)

121mm x 121mm x 75.5 mm

Weight

0.8 kg

Data interface

CAN Bus, RS-232, USB via I/O module

Position

No local frame definition available.

Data logging, storage and archiving

Logged parameter

No parameters available.

Rawdata storage on board

During flight AIMMS20 data are stored on a USB drive.

Data archiving on land

After the flight AIMMS20 data are made accessible within the external devices file system of the aircraft data managment system (DMS).

Documentation

No resources available.

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


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