Introduction
ER-MIMU-M06 Micro-Inertial Integrated Chip is an ultra-small, ultra-low power consumption chip IMU, internal integration of three-axis gyro and three-axis accelerometer, with high precision, high reliability and so on.
Features
Six-axis integration
Ceramic packaging
Ultra small size
Ultra-low power consumption
Integrated temperature sensor
Resistant to 10000g impact
Application
Inertial navigation: Inertial guidance,Integrated navigation, Stabilization of platforms
Short-term navigation:Flight control, Attitude correction, Telemetry and remote control
Attitude control:UAV, Antenna positioning
Specifications
Test conditions: room temperature (23±2℃), Vdd=3.3V
Description: gyro range ±500°/s~±4000°/s optional
Item | Parameter | Unit |
Gyroscope | ||
Range | ±500 | º/s |
Scale Factor Non-Linearity | 100 | ppm |
Angular Random Walk | 0.21 | º/√h |
Bias Instability | 2 | º/h |
Bias stability (1σ) | 20 | º/h |
Bias Repeatability (1σ) | 10 | º/h |
Bandwidth(optional) | ≥150 | Hz |
Accelerometer | ||
Range | ±10 | g |
Scale Factor Non-Linearity(±1g) | 200 | ppm |
Angular Random Walk | 0.025 | m/s/√h |
Bias Instability | 0.025 | mg |
Bias stability (1σ) | 0.1 | mg |
Bias Repeatability(1σ) | 0.1 | mg |
Bandwidth(optional) | ≥150 | Hz |
Electrical specification | ||
Operating Voltage | 3.3±0.3 | V |
Operating Temperature | -40~105 | ℃ |
Shock Resistance | 10000 | g |
Vibration | 8 | gRMS |
Dimension | 5×5×1.8mm | / |
Weight | <0.15 | g |
Interface protocol | SPI | / |
Interface Definition
No. | Definition |
1,10,15 | VDD |
2 | CS |
3 | SCLK |
5 | MOSI |
9,11,12,14,16 | GND |
13 | MISO |
4,6,7,8 | N.C. |
Dimensions
Application Techniques
1.IMU working principle & Tactical grade IMU product recommendations
2.Choosing an IMU: FOG IMUs vs MEMS IMUs
3.Application of IMU in the Field of Drones
5.What is the Difference Between IMU and AHRS?