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Note
titleAttention:

The same inertial reference 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.

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Sensorweb integration
urnaircraft:bt-67:ins
contenttypeMetadata


ManufacturerHoneywell
ModelLaseref V
Serial No.n/a
Typeinertial navigation system



Sensorweb integration
urnaircraft:bt-67:ins
contenttypeImages



Contacts

Sensorweb integration
urnaircraft:bt-67:ins
contenttypeContacts


Martin Gehrmann
NameInstitutionRole
Martin Gehrmann
Editor

Device Contact



Available devices and Specifications

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urnaircraft:bt-67:ins
contenttypeSubdevices


NameModelType
Inertial Reference System P5Laseref Vinertial navigation system
Inertial Reference System P6Laseref Vinertial navigation system



Specifications of KT19.85II (without mounting)

Metadata list
|| 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||

Position

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contenttypeLocalFrame


Origin Description:
The inertial reference system is installed in the
cockpit
.



Data logging, storage and archiving

Logged parameter

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urnaircraft:bt-67:ins
contenttypeParameters


ParameterSensor Output TypeUnit
East West Velocityspeedknots
Ground Speedspeedknots
Inertial Altitudealtitudeft
Inertial Vertical Speedspeedft
latitudelatitudedecimal degrees
longitudelongitudedecimal degrees
Magnetic headingdirectiondegree
North South Velocityspeedknots
Pitch Angleattitudedegree
Roll Angleattitudedegree
True Headingdirectiondegree
True Track Angleattitudedegree
Vertical Accelerationaccelerationg
Wind Directiondirectiondegree
Wind Speedspeedknots
X Accelerationaccelerationg
Y Accelerationaccelerationg
Z Accelerationaccelerationg


Rawdata storage on board

Metadata (Metadata Plugin)
0Rawdata
During flight INS data are stored within the aircraft onboard DMS system.

Data archiving on land

Metadata (Metadata Plugin)
0DataOnLand
After the flight INS data are accessible via the land system of the aircraft data managment system (DMS).

DMS

Metadata list
|| 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 ||


Documentation

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urnaircraft:bt-67:ins
contenttypeResources



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