High-performance Navigation MEMS IMU
Introduction
The Inertial Measurement Unit (IMU) is a device that measures the three-axis attitude angles (or angular velocities) and accelerations of an object. Gyroscopes and accelerometers are the core components of an Inertial Navigation System (INS). By using the built-in accelerometers and gyroscopes, the IMU can measure the three-axis linear accelerations and three-axis rotational angular velocities, and obtain the information of the carrier's attitude, velocity and displacement through analysis. The ER-MIMU-182 uses high-quality and highly reliable MEMS accelerometers and gyroscopes.
Feature
Gyroscope bias instability: 0.03 deg/hr
Gyroscope bias stability (10s 1σ): <0.5 deg/hr
Gyroscope angle random walk: <0.025 °/√h
Accelerometer bias repeatability: 100 ug
Accelerometer second-order nonlinearity: <100 ug/g²
High-performance navigation
Application
Integrated navigation system and inertial guidance system
Flight control system
Attitude and heading reference system (AHRS)
Stability of antennas, cameras and platforms
Aeronautical and marine geographic surveying / mapping
Specification
Project | Parameter | Unit | |
Gyroscope | A | B | / |
Range | 300 | 400 | deg/s |
Scale factor(25°C) | 28000 | 20000 | LSB/deg/s |
Scale factor repeatability of (1σ) | <50 | <20 | ppm |
Scale factor temperature drift (1σ) | ±300 | ±100 | ppm |
Scale factor non-linearity (1σ) | <300 | <100 | ppm |
Bias instability (1σ at 25°C) | 0.03 | 0.03 | deg/hr |
Bias stability (10s at 1σ) | <0.15 | <0.5 | deg/hr |
Angle random walk | <0.01 | <0.025 | °/√h |
Bias repeatability (1σ at 25°C) | <0.3 | <0.15 | deg/hr |
Accelerometer | |||
Range | 30 | g | |
Bias stability (10s 1σ) | <50 | ug | |
Bias monthly repeatability (1σ) | 100 | ug | |
Bias temperature coefficient | <20 | ug/℃ | |
Bias temperature hysteresis | <1.5 | mg | |
Scale factor non-linearity | <500 | ppm | |
Scale factor monthly repeatability | <30 | ppm | |
Scale factor temperature coefficient | 10 | ppm/℃ | |
Scale factor ClassⅡnon-linearity coefficient | <100 | ug/g² | |
Scale factor | 250000 | Lsb/g |
Application Techniques
1.Do you know the core components that give precise control to automated equipment
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6.From flight control to fault diagnosis, how does IMU dominate drones?