ER-MIMU-M02A Low Cost Inertial Measurement Unit
Introduction
ER-MIMU-M02A is an inertial measurement unit (IMU) based on micro-mechanical technology (MEMS). It is a complete inertial system with a built-in three-axis gyroscope and a three-axis accelerometer to measure the three-axis angular parameters of the carrier, such as speed, acceleration, etc. The output data after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) can be solved to obtain information such as carrier attitude, speed, displacement, etc. It also has a built-in three-axis magnetic sensor and air pressure sensor.
Features
Three-axis digital gyroscope:
Dynamic measurement range: ±450º/s;
Bias instability: 0.3 º/h (Allen variance);
Angle random walk: 0.15º/√h.
Three-axis digital accelerometer:
Dynamic measurement range: ±20g;
Bias stability: 2ug (Allen variance);
Angular Random Walk: 0.005m/s√h;
Ensure accuracy over the full temperature range (-40°C~80°C): Built-in high-performance temperature calibration and compensation algorithm;
Communication interface: 1 SPI
Application
unmanned aerial vehicles, aerial photography, agricultural plant protection, photoelectric detection stability;vehicle navigation, vehicle satellite communications, forest and land monitoring, high-speed railway track inspection; hydrological Measurement, waterway detection, shipboard positioning communication, unmanned surface vehicle.
Specifications
Parameter | Test condition | Min value | Typical value | Max value | Unit |
Gyroscope | |||||
Measuring range | ±450 | º/s | |||
Bias stability | 1s smoothing, rms | 10 | º/h | ||
Bias instability | Allan variance | 0.3 | º/h | ||
Random Walk | 1б | 0.15 | º/√h | ||
Bias Repeatability | 1б | 10 | º/h | ||
Full temperature bias | -40 ~ 80 °C, 10s smoothing | 0.01 | º/s | ||
Scale factor non-linearity | FS=450 º/s | 0.03 | %FS | ||
Bandwidth(3dB) | 250 | Hz | |||
Accelerometer | |||||
Measuring range | ±20 | g | |||
Bias stability | Allan variance | 2 | mg | ||
Random Walk | 1б | 0.005 | m/s/√h | ||
Bias Repeatability | 1 σ | 5 | mg | ||
Full temperature bias | -40 ~ 80 °C, 10s smoothing | 5 | mg | ||
Scale factor non-linearity | FS=8g | 0.1 | %FS | ||
Bandwidth | 250 | Hz | |||
Magnetometer | |||||
Dynamic measurement range | ±2.5 | Gauss | |||
Resolution | 120 | uGauss | |||
Noise Density | 50 | uGauss | |||
Bandwidth | 200 | Hz | |||
Barometer | |||||
Pressure range | 450 | 1100 | mbar | ||
Overall error | 6 | ||||
Resolution | 0.1 | mbar | |||
Absolute measurement accuracy | 1.5 | mbar | |||
Long-term stability | ±1 | mbar/yr | |||
Communication Interface | |||||
1 way SPI | Baud rate | 15 | MHz | ||
Electrical specification | |||||
Voltage | 2.5 | 3.3 | 12 | V | |
Power dissipation | 1.5 | W | |||
Ripple wave | P-P | 100 | mV | ||
Structural characteristics | |||||
Dimension | 47×44×14mm | ||||
Weight | 50 | g | |||
Operating environment | |||||
Operating temperature | -40 | 80 | ℃ | ||
Storage temperature | -45 | 85 | ℃ | ||
Vibration | 6.06g,10~2000Hzs | ||||
Impact | 2000g,0.1ms |
Application Techniques
1.IMU working principle & Tactical grade IMU product recommendations
3.Choosing an IMU: FOG IMUs vs MEMS IMUs
4.Application of IMU in the Field of Drones
5.What is the Difference Between IMU and AHRS?