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
Low cost
Gyroscopic bias instability: 1 deg/hr
Gyroscopic bias stability (10s 1σ): 5 deg/hr
Gyroscopic angle random walk: 0.25 °/√h
Application
Autonomous machine control and positioning in autonomous robots and unmanned vehicles
Azimuth, attitude and position measurement and stabilization in GNSS-assisted INS
Pitch and roll measurement in UAV AHRS
Motion measurement and stabilization in MRU
Attitude and azimuth stabilization, and positioning in IMU
Specification
Project | Parameter | Unit | ||
Gyroscope | A | B | ||
Range | 400 | 400 | deg/s | |
Scale factor(25°C) | 20000 | 20000 | LSB/deg/s | |
Scale factor temperature drift (1σ) | ±500 | ±500 | ppm | |
Scale factor non-linearity (1σ) | <200 | 200 | ppm | |
Bias instability (1σ at 25°C) | 3 | 1 | deg/hr | |
Bias stability (10s at 1σ) | 5 | 4 | deg/hr | |
Angle random walk | <0.25 | <0.2 | °/√h | |
Bias repeatability (1σ at 25°C) | 5 | 4 | deg/hr | |
Accelerometer | ||||
Range | ±10,±20, ±40 | g | ||
Cross-coupling sensitivity | 1 | % | ||
Scale factor | ±10, ±20, ±40 | 19.5, 39, 78 | ug/LSB | |
Sensitivity temperature coefficient | ±0.01 | %/°C | ||
Repetition | X, Y axis, Z axis | 0.1, 0.2 | % | |
Non-linearity | ±10g, ±40g | 0.1, 1.3 | % FSR | |
Spectral density | ±10, ±40 | 75, 90 | ug/√Hz | |
Random walk of velocity | X, Y axis Z axis | 38.2, 26.5 | mm/sec/√Hr | |
Low-pass filter bandwidth | 0.977-1000 | Hz |
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?