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Comment: Automatically updated by Registry2Confluence-Transporter (aircrafts@ingestsrv1, ask o2a-support@awi.de for questions)

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Note
titleAttention:

The same inertial reference system is systems are installed permanently on Polar 5 and Polar 6.

Summary

Sensorweb integration
urnaircraft:bt-67:ins
contenttypeSummary

KT19.85II is a remote-sensing thermometer used to determine the temperature of a surface from the distance by measuring the amount of thermal radiation emitted from the surface. KT19.85II is operates in the spectral range of 9.6 - 11.5 µm. Data are stored within the DMS framework on ADA-C1An inertial ravigation system is a navigation device that uses a computer, motion sensors (accelerometers) and rotation sensors (gyroscopes) to continuously calculate by dead reckoning the position, the orientation, and the velocity (direction and speed of movement) of a moving object without the need for external references.


Sensorweb integration
urnaircraft:bt-67:ins
contenttypeMetadata
Manufacturer
Heitronics
Honeywell
Model
KT19.85II
Laseref V
Serial No.n/a
Type
thermometer
inertial navigation system
REGISTRY-Link↪ REGISTRY (6284)


Sensorweb integration
urnaircraft:bt-67:ins
contenttypeImages

Image Removed Image RemovedImage Added

Contacts

Sensorweb integration
urnaircraft:bt-67:ins
contenttypeContacts
Name Institution Role
Gerit Birnbaum
Martin GehrmannAlfred
-Wegener-Institut
Wegener Institute, Helmholtz Centre for Polar and Marine ResearchDevice Contact


Available devices and Specifications

Sensorweb integration
urnaircraft:bt-67:ins
contenttypeSubdevices
Name Model
Type
Radiation thermometer KT19.85IIKT19.85IIthermometer
Radiation thermometer KT19.85IIKT19.85IIthermometer

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Serial Number REGISTRY-Link
Inertial Reference System P5Laseref Vn/a↪ REGISTRY (6285)
Inertial Reference System P6Laseref Vn/a↪ REGISTRY (6621)


Specifications of Laseref V (without mounting)

Metadata list
|| Dimension KT19.85II (L x W x H)| 237 x 66 x 138 mm ||
|| Weight KT19.85II | 2.35 kg||
|| Power Supply| 22 - 30 VDC ||
|| Data interface | analog output (0-20mA) and serial interface (RS232)||
Position
 Sensorweb integration
urnaircraft:bt-67:ins
contenttypeLocalFrame
InfoThe Inertial Reference System is installed in the cockpit.
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
 Sensorweb integration
urnaircraft:bt-67:ins
contenttypeParameters
 Parameter 
Sensor 
 O2ARegistry Output Type  Unit 
surface temperaturetemperature°C
East West Velocityspeedknot
Ground Speedspeedknot
Inertial Altitudealtitudeft
Inertial Vertical Speed speedft
latitudelatitudedeg
longitudelongitudedeg
Magnetic headingdirectiondeg
North South Velocityspeedknot
Pitch Angleattitudedeg
Roll Angleattitudedeg
True Headingdirectiondeg
True Track Angleattitudedeg
Vertical Accelerationaccelerationg
Wind Directiondirectiondeg
Wind Speedspeedknot
X Accelerationaccelerationg
Y Accelerationaccelerationg
Z Accelerationaccelerationg
surface temperature rawtemperaturemA
Rawdata storage on board
 Metadata (Metadata Plugin)
0Rawdata
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).
 Metadata (Metadata Plugin)
0DataOnLand
DMS
 Metadata list
|| 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
 Sensorweb integration
urnaircraft:bt-67:ins
contenttypeResources