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Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output

Categories IMU Accelerometer Gyro
Brand Name: Firepower
Model Number: IMU6-1
Place of Origin: China
MOQ: 1
Price: 2000$
Payment Terms: L/C,D/A,D/P,T/T,Western Union
Supply Ability: 500/month
Delivery Time: 1 Week for sample
Packaging Details: BOX+Sponge
Gyro Measuring range: ±400°/s
Bias Stability: 0.3°/h
Angular Random Walk: 0.15º/√h
Bias repeatability (1σ ): 1°/h
Scale Factor Repeatability (1σ ): 150ppm
3 dB Bandwidth: 250Hz
Accelerometer bias stability: 0.02mg
Weight: 55g
Misalignment: ±0.05°
Power consumption: 2W
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Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output

Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output
Key Specifications
AttributeValue
Gyro Measuring range±400°/s
Bias Stability0.3°/h
Angular Random Walk0.15º/√h
Bias repeatability (1σ)1°/h
Scale Factor Repeatability (1σ)150ppm
3 dB Bandwidth250Hz
Accelerometer bias stability0.02mg
Weight55g
Misalignment±0.05°
Power consumption2W
Product Overview

The IMU6 MEMS Inertial Measurement Unit is a highly integrated sensing system that combines:

  • Three-axis gyroscope
  • Three-axis accelerometer
  • Three-axis inclination angle sensor
  • Temperature sensor
  • Signal processing board
  • Mechanical housing
  • Accompanying software

Designed to measure three-axis angular rate, linear acceleration, and inclination angle of moving platforms, the system features comprehensive error compensation including temperature compensation, installation misalignment correction, and nonlinear compensation.

Outputs high-accuracy data via standard RS-422 serial interface following predefined communication protocol.

Technical Specifications
Gyroscope Specifications
ParameterUnitIMU6-1IMU6-1AIMU6-1BIMU6-1C
Measuring range (customizable)°/s±400±400±400±2000
In-Run Bias Stability(@ Allan variance)°/h0.30.10.051
Bias stability @10s (10s smooth, 1σ, room temperature)°/h310.56
Bias stability in full temperature°/h103218
Angular Random Walk°/√h0.150.10.020.3
Bias repeatability (1σ)°/h10.50.32
Bias acceleration sensitivity°/h/g1112
Scale Factor Non-Linearity(1σ)ppm150150150300
Scale Factor Repeatability (1σ)ppm202020100
Misalignment°±0.05±0.05±0.05±0.05
3 dB BandwidthHz250200150250
Accelerometer Technical Indicators
ParameterUnitIMU6-1y-1IMU6-1y-2IMU6-1y-3IMU6-1y-4
Measuring range (customizable)g±10±30±50±80
In-Run Bias Stability (Allan Variance @ 25 ℃)mg0.020.050.10.2
Bias stability @10smg0.050.20.51
Bias stability in full temperaturemg13515
Angular Random Walkm/s/√h0.0010.0020.0050.01
Bias repeatability(1σ)mg0.10.512
Scale Factor Repeatability (1σ)ppm200200200200
Scale Factor Non-Linearity(1σ)ppm50100200300
Misalignment°±0.05±0.05±0.05±0.05
3 dB BandwidthHz100100100100
Tilt Angle Specification (Optional)
ParameterUnitIMU6-1y-x
Measuring range (customizable)g±1.7
Bias stability (1s smoothing)mg0.5
Random walkm/s/√h0.08
Scale factor non-linearityppm100
Electrical Characteristics
ParameterUnitIMU6-1y-x
VoltageV5
Power consumptionW2
RipplemV100
Environmental Adaptability
ParameterUnitIMU6-1y-x
Operating temperature-45~85
Storage temperature-55~105
Vibration--10~2000Hz,6.06g
Impact--1000g,0.1ms
Weightg55±5
Outline Structure
IMU6 Inertial Measurement Unit outline structure diagram
Quality Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output for sale
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