ER-MIMU-05 High Accuracy North-Seeking MEMS IMU
Introduction
ER-MIMU-05 is the world’s smallest six axis MEMS IMU. Inertial Measurement Unit, referred to as IMU, is a device to measure the attitude angle (or angular velocity) and acceleration of the three axis of the object. With the built-in accelerometer sensor and gyroscope, the IMU can measure the linear acceleration and rotation angular velocity from three directions and can obtain the attitude, velocity and displacement information of the carrier through the resolving.
Features
Smallest Size: 38.6mm x 44.8mm x25.5mm
Range can be selected
Light weight: ≤70g
Temperature compensation: -40℃~ + 80℃
Products with wide voltage design: 6v~12v
Gyro bias instability up to: <0.01 deg/hr
Gyro bias stability up to (10s 1σ): <0.05 deg/hr
Gyro angular random walk up to: <0.0025 °/√h
Accelerometer bias repeatability: 100ug
Accelerometer bias stability (10s 1σ): <50ug
Accelerometer class II non-linearity coefficient: <100ug/g2
6V power supply, low power consumption 2W
RS422 bus communication, baud rate from 230400~921600 can be set
Application
Initial alignment in UAV launch systems
Guidance and navigation in navigation grade MEMS system
Orientating and positioning in railway train system
Precision platform attitude measuring and controls
Precision attitude, position measuring in navigation grade MEMS IMU/INS
North finding and positioning in land surveying/land mobile mapping system
Bridge, tall building, tower, dam monitoring
Rock and soil monitoring
Specifications
Item | Parameter | Unit | ||
Gyro performance | A | B | C | / |
Range | 50 | 100 | 200 | deg/s |
Scale Factor at 25°C | 160000 | 80000 | 40000 | LSB/deg/s |
Scale Factor Repeatability (1σ) | <50 | <50 | <100 | ppm |
Scale Factor VS Temperature (1σ) | ±300 | ±300 | ±300 | ppm |
Scale Factor Non-Linearity (1σ) | <200 | <200 | <300 | ppm |
Bias Instability (1σ 25℃) | <0.01 | <0.02 | <0.02 | deg/hr |
Bias stability (10s 1σ) | <0.05 | <0.1 | <0.1 | deg/hr |
Angular Random Walk | <0.0025 | <0.005 | <0.005 | °/√h |
Bias Repeatability (1σ 25℃) | <0.1 | <0.1 | <0.1 | deg/hr |
Accelerometer performance | ||||
Range | 30 | g | ||
Bias Stability (10s 1σ) | <50 | ug | ||
Bias Month Repeatability(1σ) | 100 | ug | ||
Bias Temp Coefficient | <20 | ug/℃ | ||
Bias Temp Hysteresis | <1.5 | mg | ||
Scale Factor Non-linearity | <500 | ppm | ||
Scale Factor Month Repeatability | <30 | ppm | ||
Scale Factor Temp Coefficient | 10 | ppm/℃ | ||
Class II Non-linearity Coefficient | <100 | ug/g2 | ||
Scale Factor | 250000 | Lsb/g | ||
Environment and power | ||||
Operate temperature | -40~+80 | ℃ | ||
Storage temperature | -55~+105 | ℃ | ||
Power supply | 6~12V | V | ||
Power | 2 | W | ||
Communication interface | RS-422 | |||
Physical characteristics | ||||
Size | 38.6 x 44.8 x 25.5 | mm | ||
Weight | ≤70 | g |
Dimension
Application Techniques
2.What is the Difference Between IMU and AHRS?
4.Application of IMU in the Field of Drones
5.Choosing an IMU: FOG IMUs vs MEMS IMUs
6.IMU working principle & Tactical grade IMU product recommendations