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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
contenttypeMetadata
ManufacturerHoneywell
ModelLaseref V
Serial No.n/a
Typeinertial navigation system
SENSORREGISTRY-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 -InstituteInstitute, Helmholtz Centre for Polar and Marine ResearchDevice Contact


Available devices and Specifications

Sensorweb integration
urnaircraft:bt-67:ins
contenttypeSubdevices
Name Model Serial Number SENSOR REGISTRY-
Link
Inertial Reference System P5Laseref Vn/a↪ REGISTRY (6285)
Inertial Reference System P6Laseref Vn/a↪ REGISTRY (6621)


Specifications of Laseref V (without mounting)

|| Dimension (L x W x H)| 165 x 163 x 163 mm || || Weight | 4.5 kg|| || Power Supply| 22 - 30 VDC || || Data interface | ARINC 429||
Metadata list
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
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 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
...
 Metadata (Metadata Plugin)
0Rawdata
During flight INS data are stored within the aircraft onboard DMS system.
Data archiving on land
After the flight INS data are accessible via the land system of the aircraft data managment system (
 Metadata (Metadata Plugin)
0DataOnLand
DMS
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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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