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IMU570 INS Inertial Measurement Sensor System Triaxis 10g Vibration

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Shenzhen Rion Technology Co., Ltd.

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IMU570 INS Inertial Measurement Sensor System Triaxis 10g Vibration

Country/Region	china
City & Province	shenzhen
Categories	Measuring & Analysing Instrument Processing Services

Product Details

IMU570 low cost IMU/INS navigation system/IMU/GPS from china RION brand

Introduction

IMU570 inertial navigation unit is composed of three-axis gyroscope, three-axis acceleration, temperature sensor and signal processing circuit. The three-axis angular rate of the carrier is measured, and the three angular rate data after error compensation (including temperature compensation, installation misalignment compensation, non-linear compensation, etc.) are output through RS422 serial port according to the agreed communication protocol. The product adopts differential gyroscope structure, effectively restrains the influence of linear acceleration and vibration, and adopts full temperature compensation to suit the harsh environment of industrial application.

Feature

★ measure triaxial angular velocity of carrier ★ working temperature:-40~85℃

★ storage temperature :-40~85℃ ★ Vibration:10~2000Hz,10g

★ power supply :+5±0.5V(DC) ★ impact:100g@11ms,Triaxial (half sinusoidal)

Application

★ Autopilot Vehicle ★ Unmanned Aerial Vehicle ★AGV

★ SOTM attitude unit ★ POS System for Surveying and Mapping

★ Ship and Marine Engineering ★ Ocean and Underwater Surveying and Mapping

★ Flight Control System ★ High Speed Train Measurement and Control System

Detailed Images

IMU570					Parameters
GYRO
Measuring range					1800°/s
Zero bias instability(@Allan variance)					≤8°/h(-20~70 ℃)
angle random walk(@Allan variance)					≤0.13°/√h & 0.24°/√h
Zero Bias Acceleration Sensitivity					≤1°/h/g
Resolution					≤0.001°/s
Scale factor nonlinearity					≤100ppm
Scale factor repeatability					≤100ppm
Cross-coupling					≤0.1%
Bandwidth					≥200Hz
Accelerometer
Measuring range					±38g
Zero bias instability(@Allan variance)					0.019mg
Zero bias repeatability					0.08mg
Speed random walk(@Allan variance)					0.04m/s/√h
Zero Bias Error in Full Temperature Range					0.5mg
Weight					(52±5)g
Other parameters
Power supply voltage					(+5±0.5)V(DC)
Power supply Current					Working current＜0.3A
Working temperature					-40~85℃
Storage temperature					-40~85℃
Vibration					10~2000Hz,10g
Impact					100g@11ms,Triaxial (half sinusoidal))

Note:

Synchronization signals need to be specially configured according to requirements. The default IMU

integrated inertial navigation system has not this configuration and needs to be suspended.

B) Reset signals need to be specially configured according to requirements. The default IMU integrated inertial navigation system has not this configuration and needs to be suspended.

External trigger sources need to be specially configured according to requirements. The default IMU integrated inertial navigation system has not this configuration and needs to be suspended.

▶ Space coordinate system

Right Hand Rule Principle 1

IMU570 contains three DOF gyroscopes, representing three axes of spatial coordinate system, namely X, Y and Z. The X axis positive is directed forward from the connector to the middle mounting hole of the sticker, the Y axis positive is directed right to the IMU, and the Z axis positive is directed downward to the bottom of the IMU, as shown in Figure 1.