Micro-Inertial Integrated Chip

ER-MIMU-M06 (2 deg/hr)
1. 3 axis gyroscope & 3-axis accelerometer;
2. Operate Temp:-40℃~ + 105℃;
3. Gyro bias instability: 2 deg/hr.

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Introduction

ER-MIMU-M06 Micro-Inertial Integrated Chip

Introduction
ER-MIMU-M06 Micro-Inertial Integrated Chip is an ultra-small, ultra-low power consumption chip IMU, internal integration of three-axis gyro and three-axis accelerometer, with high precision, high reliability and so on.

Features
Six-axis integration
Ceramic packaging
Ultra small size
Ultra-low power consumption
Integrated temperature sensor
Resistant to 10000g impact

Application
Inertial navigation: Inertial guidance,Integrated navigation, Stabilization of platforms
Short-term navigation:Flight control, Attitude correction, Telemetry and remote control
Attitude control:UAV, Antenna positioning

Specifications
Test conditions: room temperature (23±2℃), Vdd=3.3V
Description: gyro range ±500°/s~±4000°/s optional

Item	Parameter	Unit
Gyroscope
Range	±500	º/s
Scale Factor Non-Linearity	100	ppm
Angular Random Walk	0.21	º/√h
Bias Instability	2	º/h
Bias stability (1σ)	20	º/h
Bias Repeatability (1σ)	10	º/h
Bandwidth(optional)	≥150	Hz
Accelerometer
Range	±10	g
Scale Factor Non-Linearity(±1g)	200	ppm
Angular Random Walk	0.025	m/s/√h
Bias Instability	0.025	mg
Bias stability (1σ)	0.1	mg
Bias Repeatability(1σ)	0.1	mg
Bandwidth(optional)	≥150	Hz
Electrical specification
Operating Voltage	3.3±0.3	V
Operating Temperature	-40~105	℃
Shock Resistance	10000	g
Vibration	8	gRMS
Dimension	5×5×1.8mm	/
Weight	＜0.15	g
Interface protocol	SPI	/