Miniaturized MEMS IMU
Introduction
The product is mainly composed of three-axis MEMS accelerometer and gyroscope. The working principle is as follows: the gyroscope and accelerometer data are collected by ARM microcontroller, three high-precision gyroscopes are collected by 1-channel digital interface SPI, and three accelerometers are collected by another 1-channel digital interface SPI. All sensors are calibrated and compensated in software after acquisition.
Features
Mini diameter:120mm x Φ30mm
Light weight: ≤150g
Temperature compensation: -40℃~ + 80℃
Products with wide voltage design: 6v~12v
Gyro bias instability: <0.3deg/hr
Gyro bias stability (10s 1σ): <3deg/hr
Gyro angular random walk: <0.125°/ √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
Azimuth, attitude, position measuring and keeping in GNSS-assisted INS
Heading, pitch, roll measuring in AHRS for UAV
Motion survey and keeping in MRU
Attitude & azimuth keeping, positioning in IMU
Stabilizing & Pointing in satellite antenna, target tracking system
Robotic Control & Orientation in autonomous machines
Unmanned vehicles
Specifications
Item | Parameter | A | B | C | Unit |
Gyro performance | |||||
Range | 400 | 400 | 400 | deg/s | |
Scale Factor at 25°C | 16000 | 20000 | 20000 | LSB/deg/s | |
Scale Factor Repeatability (1σ) | <50 | <100 | <50 | ppm | |
Scale Factor VS Temperature (1σ) | ±300 | ±500 | ±500 | ppm | |
Scale Factor Non-Linearity (1σ) | <300 | <300 | <300 | ppm | |
Bias Instability(1σ 25℃) | <0.3 | <0.3 | <0.1 | deg/hr | |
Bias stability (10s 1σ) | <3 | <2 | <1 | deg/hr | |
Angular Random Walk | <0.125 | <0.125 | <0.05 | °/ √h | |
Bias Repeatability(1σ 25℃) | <3 | <2 | <1 | 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