IMU6
Inertial Navigation
Digital Output
6 Axis
0.5 Deg/H
IP67
CE
Customized
-400deg/S-+400deg/S
0.5 Deg/H
30g
0.02mg
200Hz
RS422
5V
Sponge and Box
38.6 X 44.6 X 21.5mm
9031809090
Product Description
Advanced Inertial Measurement Units (IMUs) High-accuracy Motion Sensing Unit
This instruction manual is the main reference document for the use and operation of IMU6-1, and is mainly prepared in accordance with the Technical Agreement of IMU6-1 MEMS Inertial Measurement Unit and the Technical Conditions of Inertial Measurement Unit and Triaxial Gyro Combination. IMU6-1 series inertial measurement unit can change the measurement accuracy and measurement range of the inertial sensor according to the user's requirements.
Composition and function 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.
Gyroscope specifications
Acc Specifications
Size
Company and production line
This instruction manual is the main reference document for the use and operation of IMU6-1, and is mainly prepared in accordance with the Technical Agreement of IMU6-1 MEMS Inertial Measurement Unit and the Technical Conditions of Inertial Measurement Unit and Triaxial Gyro Combination. IMU6-1 series inertial measurement unit can change the measurement accuracy and measurement range of the inertial sensor according to the user's requirements.
Composition and function 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.
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 |
Size
Company and production line