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

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

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
Key Specifications
Attribute Value
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
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
Parameter Unit IMU6-1 IMU6-1A IMU6-1B IMU6-1C
Measuring range (customizable) °/s ±400 ±400 ±400 ±2000
In-Run Bias Stability(@ Allan variance) °/h 0.3 0.1 0.05 1
Bias stability @10s (10s smooth, 1σ, room temperature) °/h 3 1 0.5 6
Bias stability in full temperature °/h 10 3 2 18
Angular Random Walk °/√h 0.15 0.1 0.02 0.3
Bias repeatability (1σ) °/h 1 0.5 0.3 2
Bias acceleration sensitivity °/h/g 1 1 1 2
Scale Factor Non-Linearity(1σ) ppm 150 150 150 300
Scale Factor Repeatability (1σ) ppm 20 20 20 100
Misalignment ° ±0.05 ±0.05 ±0.05 ±0.05
3 dB Bandwidth Hz 250 200 150 250
Accelerometer Technical Indicators
Parameter Unit IMU6-1y-1 IMU6-1y-2 IMU6-1y-3 IMU6-1y-4
Measuring range (customizable) g ±10 ±30 ±50 ±80
In-Run Bias Stability (Allan Variance @ 25 ℃) mg 0.02 0.05 0.1 0.2
Bias stability @10s mg 0.05 0.2 0.5 1
Bias stability in full temperature mg 1 3 5 15
Angular Random Walk m/s/√h 0.001 0.002 0.005 0.01
Bias repeatability(1σ) mg 0.1 0.5 1 2
Scale Factor Repeatability (1σ) ppm 200 200 200 200
Scale Factor Non-Linearity(1σ) ppm 50 100 200 300
Misalignment ° ±0.05 ±0.05 ±0.05 ±0.05
3 dB Bandwidth Hz 100 100 100 100
Tilt Angle Specification (Optional)
Parameter Unit IMU6-1y-x
Measuring range (customizable) g ±1.7
Bias stability (1s smoothing) mg 0.5
Random walk m/s/√h 0.08
Scale factor non-linearity ppm 100
Electrical Characteristics
Parameter Unit IMU6-1y-x
Voltage V 5
Power consumption W 2
Ripple mV 100
Environmental Adaptability
Parameter Unit IMU6-1y-x
Operating temperature ℃ -45~85
Storage temperature ℃ -55~105
Vibration -- 10~2000Hz,6.06g
Impact -- 1000g,0.1ms
Weight g 55±5
Outline Structure
Strong Shock Vibration Inertial Measurement Unit Sensor for Aerospace Defense RS-422 Output

Product Tags:

Aerospace Defense Inertial Measurement Unit

      

Strong Shock Inertial Measurement Unit

      

RS-422 Inertial Measurement Unit

      
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