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

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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.

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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

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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 V
inertial navigation system
n/a↪ REGISTRY (6285)
Inertial Reference System P6Laseref V
n/a↪ REGISTRY (6621)
inertial navigation system


Specifications of

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Laseref V (without mounting)

|| Dimension Laseref V (L x W x H)| 165 x 163 x 163 mm || || Weight KT19.85II | 4.5 kg|| || Power Supply| 22 - 30 VDC || || Data interface | ARINC 429||
Metadata list
Position
 Sensorweb integration
urnaircraft:bt-67:ins
contenttypeLocalFrame
Origin Description:cockpit
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
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 Sensorweb integration
urnaircraft:bt-67:ins
contenttypeParameters
 Parameter 
Sensor 
 O2ARegistry Output Type  Unit 
East West Velocityspeed
knots
knot
Ground Speedspeed
knots
knot
Inertial Altitudealtitudeft
Inertial Vertical Speed speedft
latitudelatitude
decimal degrees
deg
longitudelongitude
decimal degrees
deg
Magnetic headingdirection
degree
deg
North South Velocityspeed
knots
knot
Pitch Angleattitude
degree
deg
Roll Angleattitude
degree
deg
True Headingdirection
degree
deg
True Track Angleattitude
degree
deg
Vertical Accelerationaccelerationg
Wind Directiondirection
degree
deg
Wind Speedspeed
knots
knot
X Accelerationaccelerationg
Y Accelerationaccelerationg
Z Accelerationaccelerationg
Rawdata storage on board
During flight INS data are stored within the aircraft onboard DMS system.
 Metadata (Metadata Plugin)
0Rawdata
Data archiving on land
After the flight INS data are accessible via the land system of the aircraft data managment system (DMS).
 Metadata (Metadata Plugin)
0DataOnLand
DMS
|| Module name| B700 Avionics||
|| Device name | Internal Navigation System||
|| Parameters | East West Velocity \[knots\]; East West Velocity Status; ErrorText; Ground Speed \[knots\]; Ground Speed Status; Inertial Altitude \[fts\]; Inertial Altitude Status; Inertial Vertical Speed \[ft/min\]; Intertial Vertical Speed Status; Latitude \[deg\]; Latitude Status; Longitude \[deg\]; Longitude Status; Magenitc Heading \[deg\]; Magenitc Heading Status; North South Velocity \[knots\]; North South Velocity Status Pitch Angle \[deg\]; Pitch Angle Status; Pitch Rate \[deg/s\]; Pitch Rate Status; Roll Angle \[deg\]; Roll Angle Status; Roll Rate \[deg/s\]; Roll Rate Status; Status; True Heading \[deg\]; True Heading Status; True Track Angle \[deg\]; True Track Angle Status; Vertical Acceleration \[g\]; Vertical Acceleration Status; Wind Direction \[deg\]; Wind Direction Status; Wind Speed \[knots\]; Wind Speed Status; X Acceleration \[g\]; X Acceleration Status; Y Acceleration \[g\]; Y Acceleration Status; Yaw Rate \[deg/s\]; Yaw Rate Status; Z Acceleration \[g\]; Z Acceleration Status ||
 Metadata list

Documentation
 Sensorweb integration
urnaircraft:bt-67:ins
contenttypeResources
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