Versions Compared

Old Version 4

changes.mady.by.user Aircrafts

Saved on

compared with

New Version Current

changes.mady.by.user Aircrafts

Saved on

Key

  • This line was added.
  • This line was removed.
  • Formatting was changed.
Comment: Automatically updated by Registry2Confluence-Transporter (aircrafts@ingestsrv1, ask o2a-support@awi.de for questions)

...

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

An inertial ravigation system (IRS) 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
ManufacturerHoneywell
ModelLaseref V
Serial No.n/a
Typeinertial navigation system
REGISTRY-Link↪ REGISTRY (6284)


Sensorweb integration
urnaircraft:bt-67:ins
contenttypeImages

Contacts

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


Available devices and Specifications

Sensorweb integration
urnaircraft:bt-67:ins
contenttypeSubdevices
Name Model Type Serial Number REGISTRY-Link
Inertial Reference System P5Laseref Vinertial navigation system n/a↪ REGISTRY (6285)
Inertial Reference System P6Laseref Vinertial navigation system n/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) 		Origin Description:cockpit
Data logging, storage and archiving
Logged parameter
 Sensorweb integration
urnaircraft:bt-67:ins
contenttypeParameters
 Parameter  Sensor O2ARegistry Output Type  Unit 
East West Velocityspeedknotsknot
Ground Speedspeedknotsknot
Inertial Altitudealtitudeft
Inertial Vertical Speed speedft
latitudelatitudedecimal degreesdeg
longitudelongitudedecimal degreesdeg
Magnetic headingdirectiondegreedeg
North South Velocityspeedknotsknot
Pitch Angleattitudedegreedeg
Roll Angleattitudedegreedeg
True Headingdirectiondegreedeg
True Track Angleattitudedegreedeg
Vertical Accelerationaccelerationg
Wind Directiondirectiondegreedeg
Wind Speedspeedknotsknot
X Accelerationaccelerationg
Y Accelerationaccelerationg
Z Accelerationaccelerationg
Rawdata storage on board
During flight KT19.85II data are stored within the aircraft onboard DMS system.
 Metadata (Metadata Plugin)
0Rawdata
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
|| 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 ||
 Metadata list

Documentation
 Sensorweb integration
urnaircraft:bt-67:ins
contenttypeResources
...