ER-2MG-24 Ultra small size OEM Attitude Control 2 axis MEMS Gyro
Introduction
The ER-2MG-24 Ultra small size OEM attitude control 2 axis MEMS Gyro has small volume, light weight, simple structure and good reliability. The biggest function of the 2-axis gyroscope is to “measure the angular velocity to judge the motion state of the object, so it is also called a motion sensor”. In other words, this thing can let our equipment know where we are and where we are going.
Application
Construction machinery dip angle measurement, angle control, pylon operation monitoring, medical equipment angle control, satellite antenna star search, bridge, tall building, tower, dam monitoring and rock and soil monitoring, mining, attitude/heading reference system, integrated inertial navigation.
Specifications
| Parameter | ER-3MG-24 | Unit | |
| A | B | / | |
| Input Range | 400  | 400 | deg/s |
| Bandwidth(-3dB) | 200  | 200 | Hz  |
| Scale factor at 25°C | 20000  | 20000 | deg/s |
| Scale factor non-linearity(1σ) | <200  | <200  | ppm |
| Scale factor temp drift (1σ) | 500 | 500 | ppm |
| Bias instability(1σ 25℃) | 3 | 1 | deg/hr |
| Bias stability (10s 1σ) | 5 | 4 | deg/hr |
| Angular Random Walk | <0.25 | <0.2  | °/√h |
| Bias Repeatability(1σ 25℃) | 5 | 4 | deg/hr |
| Size | 40*40*42(with shell)/27*26*34(without shell and baseboard) | mm | |
| Weight | 80g(with shell)/ 40g(without shell and baseboard) | g | |
| Operate temperature | -45~+85 | ℃ | |
| Storage temperature | -55~+105 | ℃ | |
Dimension
Application Techniques
1.Error Generation Mechanism of MEMS Gyroscope Under High Acceleration Condition
2.Bandwidth test method of MEMS gyroscope
3.Packaging of MEMS gyroscope: Structural Analysis of Deep Hole Packaging
4.Research on scale factor nonlinearity of MEMS gyroscope
5.Analysis of drive loop noise of MEMS gyroscope
6.Bias Temperature Compensation Analysis of MEMS Gyroscope
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