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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 not assigned

Contacts

Name Institution Role
Martin Gehrmann Editor
Martin Gehrmann Device Contact

Available devices and Specifications

Despite the air data probe installed under the wing, the AIMMS20 system comprises AIMMS-20 modules for GPS, INS and processing permanently  installed in the underfloor compartment. An additional I/O module is installed in a rack for data storage during flight.

Name Model Type
Aircraft Integrated Meteorological Measurement System AIMMS-20 not assigned
Aircraft Integrated Meteorological Measurement System AIMMS-20 not assigned

Specifications of the air data probe AIMMS20

Dimension (L x W x H)

620 x 188 x 229 mm

Weight

23.4 kg

Power Supply

28 VDC

Data interface

CAN Bus, RS232, USB via I/O module

Position

Origin Description:The AIMMS20 is permanently installed under the right wing of the aircraft.

Data logging, storage and archiving

Logged parameter

Parameter Sensor Output Type Unit
relative humidity humidity, relative none
barometric pressure barometric pressure Pa
wind flow vector north component speed m/s
wind flow vector east component speed m/s
latitude latitude degree
longitude longitude degree
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 degree
pitch angle angular rates degree
heading angle angular rates degree
true airspeed speed m/s
vertical wind speed m/s
sideslip angle angular rates degree
angle of attack angular rates none
sideslip signal angular rates none

Rawdata storage on board

During flight KT19.85II data are stored within the aircraft onboard DMS system.

Data archiving on land

After the flight KT19.85II data are accessible via the land system of the aircraft data managment system (DMS).

DMS

Module name

B839 KT19

Device name

KT19 radiation thermometer analog

Parameters

Calibration Temperature Raw [Ohm]; ErrorText; Status; Temperature Raw [A]

Device name

KT19 radiation thermometer serial

Parameters

ErrorText; KT19 Serial; Status


Documentation


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