Low-cost MEMS IMU for Attitude Control
Introduction
ER-IMU-184 is a high-reliability and high-precision six-axis small-sized inertial measurement unit. The inertial sensing system integrates navigation-grade MEMS three-axis gyroscope and three-axis accelerometer. The angular rates and accelerations outputted are filtered and calibrated excellently, enabling ER-IMU-184 to provide precise inertial data under harsh conditions.
ER-IMU-184 offers multiple configurable industrial standard communication interfaces and a wide input voltage range, facilitating its integration into various systems. It also features a small size, low power consumption, and high precision. It is an ideal choice for attitude measurement and navigation in most marine unmanned aerial vehicle on-board applications.
Feature
Size:65*51*35.5
Weight:140
-40~80°C temperature compensation
The product is low-cost
Gyro bias instability: 1deg/hr
Gyro bias stability (10s 1σ): 4deg/hr
Gyro angular random walk: 0.2 °/√h
Accelerometer bias repeatability: 100ug
Accelerometer bias stability (10s) (1σ): <50ug
Accelerometer class II non-linearity coefficient: <100ug/g²
Application
Robotic control & orientation in autonomous machines, unmanned vehicles
Azimuth, attitude, position measuring and keeping in GNSS-assisted INS
Pitch, roll measuring in AHRS for UAV
Motion survey and keeping in MRU
Attitude & azimuth keeping, positioning in IMU
Guidance, navigation, control in tactical MEMS system
Stabilizing & Pointing in satellite antenna, target tracking system
Specification
Item | Parameter | Unit | |
Gyro performance | A | B | / |
Range | 400 | 400 | deg/s |
Scale Factor at 25°C | 20000 | 20000 | LSB/deg/s |
Scale Factor VS Temperature (1σ) | 500 | 500 | ppm |
Scale Factor Non-Linearity (1σ) | <200 | 200 | ppm |
Bias Instability (1σ 25℃) | 3 | 1 | deg/hr |
Bias Stability (10s 1σ) | 5 | 4 | deg/hr |
Angular Random Walk | <0.25 | <0.2 | °/ √h |
Bias Repeatability (1σ 25℃) | 5 | 4 | 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 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 (power supply 6V) | 2 | W | |
Communication interface | RS-422 | ||
Physical characteristics | |||
Size | 65*51*35.5 | mm | |
Weight | 140 | g |
Dimension
Application Techniques
1.Do you know the core components that give precise control to automated equipment
2.High-performance IMU: A New Benchmark for Precise Measurement and Control
3.Industrial Versatile Tool: High Cost-Performance IMU Meets Diverse Needs
4.Flight safety secrets: The core role of high-precision IMUs in aviation
5.Revolutionizing drone navigation: How to redefine high performance and low cost
6.From flight control to fault diagnosis, how does IMU dominate drones?