Introduction
ER-3MG-301 is a high precision three-axis MEMS gyroscope with small size, light weight, low power consumption and IP68 protection. Through modeling and accurate calibration of the whole working temperature zone, it can meet the performance requirements of the gyro in the whole working temperature zone and has high environmental adaptability.
Features
Miniaturization
Low power consumption
High precision
Total temperature compensation
Application areas
Inertial navigation: inertial guidance, integrated navigation, platform stability
Short-term navigation: flight control, trajectory correction, telemetry and remote control
Attitude control: UAV, antenna orientation
Specifications
Parameters | Indicator |
Range | ±450°/s |
Full temperature bias | ≤100°/h |
Angular random walk | ≤0.15°/√h |
Bias instability | ≤2°/h |
Bias stability (1σ) | ≤8°/h |
Bias repeatability (1σ) | ≤8°/h |
Scale factor non-linearity | ≤50ppm |
Bandwidth (10~250Hz adjustable) | 150Hz |
Supply voltage | 5V±0.3V |
Operating temperature | -45°C~+85°C |
Shock resistance | ≥2000g |
Vibration | ≥20grms |
Dimension | 23mm×23mm×10mm |
Weight | ≤30g |
Interface type | RS422 |
Connector | JMC-1284Z2-JH |
Output interface wiring definition | |
VCC | Power supply positive |
GND | Power ground |
Rx+ | RS422 Receive + |
Rx- | RS422 Receive - |
Tx- | RS422 Send - |
Tx+ | RS422 Send + |
Dimensions
Application Techniques
1.Main features of MEMS gyroscope
2.Research on scale factor nonlinearity of MEMS gyroscope
3.Analysis of drive loop noise of MEMS gyroscope
4.Basic dynamics analysis of MEMS gyroscope
5.Bias Temperature Compensation Analysis of MEMS Gyroscope
6.Error Generation Mechanism of MEMS Gyroscope Under High Acceleration Condition