The MEMS inertial measurement unit consists of a three-axis gyroscope, a three-axis acceleration meter, a three-axis inclination angle, a temperature sensor, a signal processing board, a structure and necessary software, and is used for measuring three-axis angular rate, three-axis acceleration and three-axis inclination angle of a carrier. And output that gyro, the loading table and the inclination data aft error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation and the like) through an RS-422 serial port according to an agreed communication protocol.
Technical Parameter
Gyroscope specifications
Parameter
Unit
IMU6-1
IMU6-1A
Measuring range (customizable)
°/s
±400
±400
Zero bias stability (@ Allan Variance)
°/h
1
0.5
Zero bias stability (1s smooth, 1σ, room temperature)
°/h
10
5
Zero bias stability (10s smooth, 1σ, room temperature)
°/h
5
1
Zero-bias error over full temperature range
°/h
20
10
Random walk
°/√h
0.2
0.1
Zero-bias repeatability
°/h
10
5
Zero bias acceleration sensitivity
°/h/g
1
1
Resolution
°/h
2
1
Scale factor nonlinearity
ppm
500
Scale factor repeatability
ppm
500
Cross coupling
%
0.1
Bandwidth
Hz
125
Acc Specifications
Parameter
Unit
IMU6-1y-1
IMU6-1y-2
Measuring range (customizable)
g
±10
±30
Zero-bias stability (Allan Variance @ 25 ºC)
mg
0.02
0.05
Zero-bias stability (1s smoothing)
mg
0.1
0.5
Zero-bias stability (10 s smoothing)
mg
0.05
0.2
Zero-bias error over full temperature range
mg
1
3
Random walk
m/s/√h
0.001
0.002
Zero-bias repeatability
mg
0.1
0.5
Scale factor repeatability
ppm
500
Scale factor nonlinearity
ppm
500
Bandwidth
Hz
125
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Outline Drawing
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