Low Power Inertial Measurement Unit
Introduction
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 rapid development of science and technology, MEMS IMU is increasingly widely used in the fields of oil and mining, injecting new vitality into this traditional industry. This is a high-performance product specially designed for oil drilling, mining and other fields. Based on three-axis integrated MEMS gyro and three-axis accelerometer, ER-MIMU-10 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
Mini diameter: 120mm x Φ30mm
Light weight: ≤150g
Temperature compensation: -40℃~ + 80℃
Products with wide voltage design: 6v~12v
Gyro bias instability: 0.05deg/hr
Gyro bias stability (10s 1σ): <0.5deg/hr
Gyro angular random walk:<0.025 °/√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
Antenna and Line of Sight Stabilization Systems
Integrated Navigation Systems & Inertial Guidance System
Flight Control & Guidance System
Attitude Heading Reference Systems (AHRS)
Stabilization of Antennas, Cameras & Platforms
Aerial and Marine Geo-mapping / Surveying
Specifications
Item | Parameter | A | B | Unit |
Gyro performance | ||||
Range | 300 | 400 | deg/s | |
Scale Factor at 25°C | 28000 | 20000 | LSB/deg/s | |
Scale Factor Repeatability (1σ) | <50 | <20 | ppm | |
Scale Factor VS Temperature (1σ) | ±300 | ±100 | ppm | |
Scale Factor Non-Linearity (1σ) | <300 | <100 | ppm | |
Bias Instability(1σ 25℃) | 0.03 | 0.05 | deg/hr | |
Bias stability (10s 1σ) | <0.15 | <0.5 | deg/hr | |
Angular Random Walk | <0.01 | <0.025 | °/ √h | |
Bias Repeatability(1σ 25℃) | <0.3 | <0.3 | deg/hr | |
Accelerometer performance | ||||
Range | 30 | g | ||
Bias Stability (10s 1σ) | <50 | ug | ||
Bias Repeatability | 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 DC | V | ||
Power (Power supply 6) | 2 | W | ||
Communication interface | RS-422 | |||
Physical characteristics | ||||
Size | 120 x Φ30 | mm | ||
Weight | ≤150 | 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