High Precision Navigation MEMS IMU

ER-MIMU-06
1. Measuring range :±400º/s;
2. Gyro bias instability: 0.05 deg/hr;
3. Gyro angular random walk:<0.025°/ √h;
4. Gyro bias stability (10s 1σ): <0.5deg/hr.

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Introduction

ER-MIMU-06 High Precision Navigation MEMS IMU

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. Gyroscope and accelerometer are the core devices of inertial navigation system (INS). With the built-in accelerometer sensor and gyroscope, the IMU 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.
ER-MIMU-06 uses MEMS accelerometer and gyroscope with high quality and reliability, RS422 and external communication, baud rate can be flexibly set between 230400~921600, through the communication protocol to set the user's required communication baud rate. With X, Y, Z three-axis precision gyro, X, Y, Z three-axis accelerometer with high resolution, can be output by RS422 X, Y, Z three axis of gyroscope and accelerometer's original hexadecimal complement data (including gyro hexadecimal complement the numerical temperature, Angle, the accelerometer hexadecimal temperature, the acceleration hexadecimal complement number); It can also output float dimensionless values of the gyroscope and accelerometer processed by the underlying calculation.

Features
Gyro bias instability:0.05deg/hr
Gyro bias stability (10s 1σ): <0.5deg/hr
Gyro angular random walk:＜0.025 °/√h
Volume:38.6mm x 44.8mm x25.5mm
6V power supply, low power consumption 2W
Light weight: ≤70g

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	Unit
Gyro performance
Range	400	deg/s
Bandwidth (-3dB)	100	Hz
Scale Factor at 25°C	20000	LSB/deg/s
Scale Factor Repeatability (1σ)	<20	ppm
Scale Factor VS Temperature (1σ)	100	ppm
Scale Factor Non-Linearity (1σ)	100	ppm
Bias Instability	0.05	deg/hr
Bias stability (10s 1σ)	<0.5	deg/hr
Angular Random Walk	<0.025	°/ √h
Bias error over temperature (1σ)	3	deg/hr
Bias temperature variations, calibrated (1σ)	<0.5	deg/hr
Bias Run-Run (1σ)	<0.3	deg/hr
Accelerometer performance
Range	30	g
Bandwidth	100	Hz
Bias Stability (1s) (1σ)	<30	ug
Bias Repeatability	200-500	ug
Bias Temp Coefficient	<20	ug/℃
Bias Temp Hysteresis	<0.5	mg
Factor Scale Non-linearity	<500	ppm
Factor Scale Repeatability	<300	ppm
Factor Scale Temp Coefficient	10	ppm/℃
Class II Non-linearity Coefficient	<100	ug/g2
Factor Scale	400000-800000	μg/LSB
System Performance
Supply Voltage	6~12V
Supply Consumption	2W
Interface	RS422
Vibration	6.06g (10~2000Hz)
Shock	5000g, 0.1ms
Operate Temp	-40℃~ + 80℃
Storage Temp	-55℃~ + 105℃
Weight	≤70g
Size	38.6mm x 44.8mm x25.5mm