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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.

Sensor-Info: aircraft:bt-67:ins, 6284

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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



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Device Contact
Sensorweb integration
urnaircraft:bt-67:ins
contenttypeContacts


NameInstitutionRole
Martin Gehrmann




Available devices and Specifications

Sensorweb integration
urnaircraft:bt-67:ins
contenttypeSubdevices


NameModelSerial Number
Inertial Reference System P5Laseref V
Inertial Reference System P6Laseref V



Specifications of Laseref V (without mounting)

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


Data logging, storage and archiving

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Sensorweb integration
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.

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