China Navigation Grade MEMS IMU  with 3 Axis Accelerometer  Gyroscope for sale
China Navigation Grade MEMS IMU  with 3 Axis Accelerometer  Gyroscope for sale
China Navigation Grade MEMS IMU  with 3 Axis Accelerometer  Gyroscope for sale
China Navigation Grade MEMS IMU  with 3 Axis Accelerometer  Gyroscope for sale
China Navigation Grade MEMS IMU  with 3 Axis Accelerometer  Gyroscope for sale
China Navigation Grade MEMS IMU  with 3 Axis Accelerometer  Gyroscope for sale
China Navigation Grade MEMS IMU  with 3 Axis Accelerometer  Gyroscope for sale

Navigation Grade MEMS IMU with 3 Axis Accelerometer Gyroscope

Navigation Grade MEMS IMU with 3-Axis Accelerometer & Gyroscope Composition and Function The inertial measurement unit integrates multiple precision sensors and processing components: Three-axis gyroscope for angular rate measurement Three-axis accelerometer for acceleration measurement Three-axis tilt angle sensor (optional) Temperature sensor for environmental compensation Signal processing board with advanced algorithms Robust mechanical structure Comprehensive software

Place of Origin China
Zero bias acceleration sensitivity 1°/h/g
Random walk 0.15。/√h
Packaging Details sponge +carton
Measuring range ±400°/s
Zero-bias repeatability 10°/h
Product Description
Navigation Grade MEMS IMU with 3-Axis Accelerometer & Gyroscope
Composition and Function

The inertial measurement unit integrates multiple precision sensors and processing components:

  • Three-axis gyroscope for angular rate measurement
  • Three-axis accelerometer for acceleration measurement
  • Three-axis tilt angle sensor (optional)
  • Temperature sensor for environmental compensation
  • Signal processing board with advanced algorithms
  • Robust mechanical structure
  • Comprehensive software suite

The system measures three-axis angular rate, acceleration, and tilt angle of the carrier, then outputs compensated data (including temperature compensation, installation misalignment compensation, and nonlinear compensation) through an RS-422 serial port using standardized communication protocols.

Gyroscope Technical Specifications
Parameter Unit Test Conditions IMU6-4 IMU6-4A IMU6-4B IMU6-4C
Measuring range °/s
±400 ±400 ±400 ±2000
Zero-bias instability °/h Allan variance 1 0.1 0.05 3
Zero bias stability °/h 1s smooth, RMS, normal temperature 10 5 1 20
Zero bias variation at full temperature °/h 10s smooth, RMS, temperature change rate 1 ℃/min 20 10 2 40
Random walk ./√h Allan variance 0.15 0.05 0.02 0.3
Zero-bias repeatability °/h Q = 6, normal temperature 10 5 1 20
Zero bias acceleration sensitivity °/h/g Test at ± 1 g 1 1 1 1
Resolution °/h
2 1 0.5 5
Output noise °/s Peak (half peak, STD * 3) 0.3 0.25 0.15 0.45
Scale factor nonlinearity ppm Normal temperature 300
Scale factor repeatability ppm Q = 3, normal temperature 300
Cross coupling % Normal temperature 0.2
Bandwidth Hz
250 250 150 250
Accelerometer Technical Specifications
Parameter Unit Test Conditions IMU6-4y-1 IMU6-4y-2 IMU6-4y
Measuring range g
±10 ±20 ±40
Zero bias stability mg 1s smooth, RMS, normal temperature 0.1 0.2 0.3
Zero bias variation at full temperature mg 10s smooth, RMS, temperature change rate 1 ℃/min 3 3 5
Zero-bias repeatability mg Q = 6, normal temperature 0.2 0.5 1
Resolution mg
0.1 0.1 0.1
Scale factor nonlinearity ppm Normal temperature 500
Scale factor repeatability ppm Q = 3, normal temperature 500
Cross coupling % Normal temperature 0.2
Bandwidth Hz
150
Inclination Angle Technical Specifications
Parameter Unit IMU6-4y-x
Measuring range g ±1.7
Zero-bias stability (1s smoothing) mg 0.5
Scale factor nonlinearity ppm 500
Electrical Characteristics
Parameter Unit IMU6-4y
Voltage V +5±0.5
Starting current mA <400
Steady-state power consumption W <1.2
Ripple mV 100
Environmental Adaptability
Parameter Unit IMU6-4y-x
Operating temperature -45~85
Storage temperature -55~105
Additional Specifications
Parameter Unit IMU6-4y-x
Weight g 55±5
Start time s 1
Outline Drawing
Navigation Grade MEMS IMU outline drawing and dimensional specifications

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