High Performance Inertial Measurement Unit LINS688B

High Performance Inertial Measurement Unit LINS688B

Main Features

– Triaxial, digital gyroscope, ±450°/sec dynamic range

– Triaxial, digital accelerometer, ±20g

– Triaxial, digital magnetometer, ±8 gauss

– Digital pressure sensor, 300 mbar to 1100 mbar

– High bandwidth 400Hz

– Factory-calibrated sensitivity, bias, and axial alignment

– Calibration temperature range: −40°C to +85°C

– SPI-compatible serial interface

– Embedded temperature sensor

– Single-supply operation: 3.0 V to 3.6 V

– 2000 g shock survivability

– Small in size and light in weight

– Fully compatible with ADIS16488A

Specification

Main Features 

– Triaxial, digital gyroscope, ±450°/sec dynamic range

– Accelerometer, ±20g

– Digital magnetometer, ±8 gauss

– Digital pressure sensor, 300 mbar to 1100 mbar

– High bandwidth 400Hz

– Factory-calibrated sensitivity, bias, and axial alignment

– Calibration temperature range: −40°C to +85°C

– SPI-compatible serial interface

– Embedded temperature sensor

– Single-supply operation: 3.0 V to 3.6 V

– 2000 g shock survivability

– Small in size and light in weight

– Fully compatible with ADIS16488A

Applications OF  the Inertial Measurement Unit 

– Anti-vibration, attitude control for industrial applications

– Autonomous machines

– Robotics control

– Platform stabilization and control

– Instrumentation

Description OF  the Inertial Measurement Unit 

Inertial Measurement Unit LINS688B is an inertial measurement device with small volume and high overload resistance. Gyro bias in-run stability is 1.5°/ h (Allan), and accelerometer bias in-run stability is 20ug (Allan). It  can be used for precise navigation, control and dynamic measurement of  carrier. This series of products use high-precision MEMS inertial devices, which have high reliability and high firmness, and can still accurately measure the angular velocity and acceleration information of the moving carrier in harsh environments.

LINS688B has a built-in three-axis gyro and three-axis accelerometer for measuring the three-axis angular rate and three-axis acceleration of the carrier. The gyro and accelerometer data with error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) are output through the serial port according to the agreed communication protocol, and the three-axis magnetic sensor and air pressure sensor are built in.

  1. Technical Specifications OF Inertial measurement unit 
ParameterTest ConditionMinNominalMaxUnit
GyroscopeRange-450+450deg/s
Bias instabilityAllan Variance1.01.52.0deg/h
Angle Random walk0.065deg/√h
Resolution0.007deg/s
NonlinearityFS = 450 °/s0.1%FS
Bandwith400Hz
AccelerometerRange-20+20g
Bias instability20μg
Velocity Random walk0.02m/s/√h
Resolution0.02mg
Nonlinearity0.1%FS
Bandwith480Hz
MagnetometerRange-8+8gauss
Resolution0.2mg
Noise density50μg
BarometerRange3001100mbar
Tolerance4.5mbar
COM interfaceSPIBaud rate<10MHzMHz
Electrical

characteristics

Voltage3.03.33.6V
Power Consumption0.5W
RippleP-P100mV
Structural

characteristics

Dimension44.0 × 47.0 ×14.0mm
Weight50g
 

 

Use

environment

Working Temperature-4075
Storage Temperature-4585
Vibration10〜2000Hz, 6g
Shock30g, 11ms
Overload(Half-sine 0.5msec)1000g
CriminalityMTBF20000h
Continuous working time120h

Related Articles:

Inertial measurement unit 

Inertial Measurement Unit (IMU) — Development & Testing

 

 

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