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Comment: Automatically updated by Sensor2Confluence-Transporter (aircrafts@ingestsrv1)

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Specifications of Laseref V (without mounting)

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|| 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||

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Sensorweb integration
urnaircraft:bt-67:ins
contenttypeLocalFrame
InfoThe Inertial Reference System is installed in the cockpit.

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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 (
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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 ||
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Documentation

Sensorweb integration
urnaircraft:bt-67:ins
contenttypeResources

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