Datasheet

2 sensing.honeywell.com
Transportation Attitude Reference System (TARS Series)
Table 1. Sensor Specifications
Characteristic Min. Typ. Max. Unit
Gyroscope 3 axis performance
Angular rate range
1
-245 +245 deg/s
Angular rate resolution 7.8125 mdps
In-run bias stability 1 mdps
Rate noise density 0.004 deg/s/sqrt Hz
Offset (0°C to 50°C) -0.8 +0.8 deg/s
Offset (-40°C to 85°C) -1.6 +1.6 deg/s
Accelerometer 3 axis performance
Acceleration range
1
-78.48 +78.48 m/s
2
Acceleration resolution 0.01 m/s
2
In-run bias stability 50 mg
Acceleration noise density 65 mg/sqrt Hz
Offset (0°C to 50°C) ±0.05 m/s
2
Offset (-40°C to 85°C) ±0.15 m/s
2
Attitude (pitch and roll) performance
Range
1
-85 +85 deg
Resolution 0.058 deg
Static error (0°C to 50°C) ±0.3 deg
Static error (-40°C to 85°C) ±0.9 deg
Translational acceleration error ±0.5 deg
Centripetal acceleration error ±0.5 deg
1
Sensors are calibrated in the following ranges: ±60 deg/s for gyroscope angular rate, ±9.81 m/s
2
for acceleration, and ±30 deg for pitch
and roll. Calibrated ranges can be extended to maximums shown with deviation to performance specifications.
Pitch and roll outputs per PGN61481 (Axes marking on the housing is Z-down convention required for pitch and roll outputs per J1939.)
Acceleration outputs per PGN61485 (Acceleration data is outputted per Z-up convention required by J1939.)
Angular rate outputs per PGN61482 (Angular rate data is outputted per Z-down convention required by J1939.)
Table 2. Electrical Specifications • TARS-LCASS Catalog Listing
Characteristic Min. Nominal Max. Unit
Supply voltage 4.5 5 5.5 V
Supply current 100 mA
Start-up time 500 2000 ms
Short circuit protection CAN output shorted to supply voltage or ground without damage
Open circuit protection Single-line interruption and multiple-line interruption
Reset response Automatic after voltage dropout
CAN output characteristics per SAE J1939
CAN Bus data rate 250 kBaud
Signal update rate 100 Hz