North-Seeking MEMS IMU for Gyro Tools

ER-MIMU-09
1. Mini Diameter: 120mm x Φ30mm;
2. Light weight: ≤150g;
3. Temperature compensation: -40℃~ + 80℃ / -40℃~ + 125℃.

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Introduction

ER-MIMU-09 North-Seeking MEMS IMU for Gyro Tools

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. With the rapid development of science and technology, MEMS IMU is increasingly widely used in the fields of oil and mining, injecting new vitality into this traditional industry. This is a high-performance product specially designed for oil drilling, mining and other fields. Based on three-axis integrated MEMS gyro and three-axis accelerometer, ER-MIMU-09 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.

Features
Mini Diameter: 120mm x Φ30mm
Light weight: ≤150g
Temperature compensation: -40℃~ + 80℃ / -40℃~ + 125℃
Products with wide voltage design: 6v~12v
Gyro bias instability up to: <0.01 deg/hr
Gyro bias stability up to (10s 1σ): <0.05 deg/hr
Gyro angular random walk up to: <0.0025 °/√h
Accelerometer bias repeatability: 100ug
Accelerometer bias stability (10s 1σ): <50ug
Accelerometer class II non-linearity coefficient: <100ug/g2
6V power supply, low power consumption 2W
RS422 bus communication, baud rate from 230400~921600 can be set

Application
North seeking in logging tools/gyro tools
Pointing, steering and guiding in advanced mining/drilling equipment
Initial alignment in UAV launch systems
Direction pointing and tracking in satellite antenna, target tracking system
Guidance and navigation in navigation grade MEMS system
Orientating and positioning in railway train system
Precision platform attitude measuring and controls
Precision attitude, position measuring in navigation grade MEMS IMU/INS
North finding and positioning in land surveying/land mobile mapping system

Specifications

Item	Parameter				Unit
Gyro performance	A	B	C	H	/
Range	50	100	200	100	deg/s
Scale Factor at 25°C	160000	80000	40000	80000	LSB/deg/s
Scale Factor Repeatability (1σ)	<50	<50	<100	<50	ppm
Scale Factor VS Temperature (1σ)	±300	±300	±300	±300	ppm
Scale Factor Non-Linearity (1σ)	<200	<200	<300	<200	ppm
Bias Instability (1σ 25℃)	<0.01	<0.02	<0.02	<0.02	deg/hr
Bias stability (10s 1σ)	<0.05	<0.1	<0.1	<0.1	deg/hr
Angular Random Walk	<0.0025	<0.005	<0.005	<0.005	°/√h
Bias Repeatability (1σ 25℃)	<0.1	<0.1	<0.1	<0.1	deg/hr
Accelerometer performance
Range	30				g
Bias Stability (10s 1σ)	<50				ug
Bias Month Repeatability(1σ)	100				ug
Bias Temp Coefficient	<20				ug/℃
Bias Temp Hysteresis	<1.5				mg
Scale Factor Non-linearity	<500				ppm
Scale Factor Month 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			-40℃~ + 125℃	℃
Storage temperature	-55~+105			-55℃~ + 125℃	℃
Power supply	6~12V DC				V
Power (Power supply 6)	2				W
Communication interface	RS-422				/
Physical characteristics
Size	120 x φ30				mm
Weight	≤150				g