High Precision Navigation/Stable Control MEMS Gyro
Introduction
The ER-3MG-03/03mini High Precision Navigation/Stable Control MEMS Gyro has small volume, light weight, simple structure and good reliability. The biggest function of the three-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-03/03mini | Unit | ||
A | B | C | ||
Range | 400 | 400 | 400 | deg/s |
Bandwidth (-3dB) | 250 | 300 | 300 | Hz |
Scale Factor at 25°C | 16000 | 20000 | 20000 | lsb/deg/s |
Scale Factor Repeatability (1σ) | <50 | <100 | <50 | ppm |
Scale Factor VS Temperature (1σ) | ±300 | ±500 | ±500 | ppm |
Scale Factor Non-Linearity (1σ) | <300 | <300 | <300 | ppm |
Bias Instability(1σ 25℃) | <0.3 | <0.3 | <0.1 | deg/hr |
Bias stability (10s 1σ) | <3 | <2 | <1 | deg/hr |
Angular Random Walk | <0.15 | <0.125 | <0.05 | °/ √h |
Bias Repeatability(1σ 25℃) | <3 | <2 | <1 | deg/hr |
Size | 70×65×45(with shell)/43.2×43.2×35.5 (without shell and baseboard)
40*40*42(mini version with shell)/27*26*34(mini version without shell and baseboard) |
mm | ||
Weight | ≤220(withshell) ≤100(without shell and baseboard)
80g(mini version with shell)/ 40g(mini version without shell and baseboard) |
g | ||
Operate temperature | -40~+80 | ℃ | ||
Storage temperature | -55~+105 | ℃ |
Dimension
Stand Version
Mini Version
Application Techniques
1.Main features of MEMS gyroscope
2.Sensitive structure analysis of MEMS gyroscope
3.The analysis of damping in MEMS gyroscope
4.The impact of turntable error on MEMS gyroscope calibration
5.How does MEMS gyroscope work in harsh high temperature environment?
6.Error Generation Mechanism of MEMS Gyroscope Under High Acceleration Condition