Low Cost MEMS Inertial Measurement Unit

Low Cost MEMS Inertial Measurement Unit

ER-MIMU-08 (≤1°/h) Features:
1. Measuring range ±400º/s;
2. Bias instability ≤1°/h;
3. Small Volume.

Low Cost MEMS Inertial Measurement Unit

Low Cost MEMS Inertial Measurement Unit

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Introduction

Low-Cost-MEMS-Inertial-Measurement-Unit for HeadingApplication of Low Cost MEMS Inertial Measurement UnitFeatures of Low Cost MEMS Inertial Measurement Unit

Low Cost MEMS Inertial Measurement Unit

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-08 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.

Application
Azimuth, attitude, position measuring and keeping In GNSS-assisted INS
Heading, pitch, roll measuring In AHRS for UAV
Motion survey and keeping in MRU
Attitude & azimuth keeping, positioning in IMU
Guidance, navigation, control in tactical MEMS weapon system
Stabilizing & Pointing in satellite antenna,target tracking system
Robotic Control & Orientation in Autonomous machines, Unmanned vehicles

Features
Volume:38.6mm x 44.8mm x25.5mm ;
6V power supply, low power consumption 2W;
Light weight: ≤70g;
Products include X, Y, Z three axis MEMS gyro and X, Y, Z three axis MEMS accelerometer;
RS422 bus communication, baud rate from 230400~921600 can be set.

Specifications

ItemParameter
Gyro Performance
Range±400°/s
Bandwidth200Hz
Scale factor20000
Scale Factor Non-linearity≤200ppm
Scale factor temp drift (1б)500 ppm
Bias instability≤1°/h
Bias Stability (10s,1σ)≤5°/h
Bias Stability (1s,1σ)≤15°/h
Bias Repeatability≤5°/h
Bias temp drift (1б)50°/h
Accelerometer Performance
Range1040g
Nonlinearity0.11.3% FSR
Cross Axis Sensitivity11%
Bandwidth2.42.4Hz
Bias Repeatability55mg
Bias Temp Coefficient<0. 5<0. 5mg/°C
Factor Scale Repeatability<0.10.2%
Factor Scale Temp Coefficient±0.01±0.01%/°C
Factor Scale800000200000μg/LSB
System Performance
Supply Voltage6V~12V
Supply Consumption2W
InterfaceRS422
Vibration6.06g (10~2000Hz)
Shock5000g, 0.1ms
Operate Temp-40℃~+ 80℃
Storage Temp-55℃~+ 105℃
Weight≤70g
Size38.6mm x 44.8mm x25.5mm


Application Techniques

1.IMU and GPS fusion algorithm principle

2.MEMS IMU error analysis and compensation

3.Reusable spacecraft IMU dynamic accuracy assessment method

4.Research on MEMS IMU error modeling and temperature compensation technology

5.Calibration method and error analysis of low-precision MEMS IMU

6.MEMS-IMU error calibration compensation method that does not rely on precision turntable


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