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Tri-Axis Inertial Measurement Unit (6DoF sensors)

PDF Catalog

1674n3ej.pdf  (1.2 MB)

This is an Inertial Sensor Unit equipped with triple axes gyroscopes and triple axes accelerometers, designed to output temperature compensated angular rate and acceleration via high speed serial lines
It also facilitates optional calculations, such as attitude, speed, angle, with the use of external data.

Applications

・Motion Guidance Control ・Platform stabilizer Control ・Navigation ・Inertial Measurement
・Camera Image Control ・Robotics ・Machine Tool

Features

MEMS_imu2_.jpg
  • Small/Lightweight/Low Power Consumption
  • Small Piezoelectric Gyro and Silicon Accelerometer
  • High-accuracy Gyro/Accelerometer
  • High Data Output Rate (200Hz)
  • Superior Environmental Resistance (Vibration/Shock)
  • Wide Temperature Range (-40°C∼85°C) (compensated by built-in temperature sensor)
  • Self Check Mechanism (Fault Detection Coverage: 95%)
  • Low Price

Function Block Diagram

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Performance Specification

Specification Value Unit(rms)
Gyro Range ±200 deg/s
Offset 0.2 deg/s
Scale Factor Error 0.5 %FS
Noise 0.5 deg/s
Accelerometer Range ±39.2(±4G) m/s2
Offset 0.098(10mG) m/s2
Scale Factor Error 0.5 %FS
Noise 0.049(5mG) m/s2
Yaw Drift 0.02 deg/s
Attitude Error 0.2 deg
Velocity/Position Calculation The hybrid navigation algorithm
is available as separate option.
External Input Information
Frequency Response 10 Hz
Maximum Update Rate 200 Hz
Warm-up period 10min
Data Format Refer : Documentation of protocol

After the offset cancellation, less than 5 minutes.

Environmental Condition

Specification Value
Power/Consumption DC7∼12V or DC4.5∼5.5V/2W max.
Temperature Range -40∼+85°C
Vibration 5.4Grms 5∼2,000Hz
Shock 200G 10ms

I/O

Specification Value
Output Line No.1 RS-232C or RS-422 115.2kpbs full duplex
Output Line No.2 CAN (2ch) (Optional)

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