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Shenzhen Rion Technology Co., Ltd.
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IMU570 10Hz MEMS Inertial Measurement Unit INS Navigation System

Product Details

Place of Origin: Guangdong, China

Brand Name: RION

Model Number: IMU570

Payment & Shipping Terms

Minimum Order Quantity: 1

Price: $548/Pieces

Packaging Details: CARTON

Delivery Time: 10 days for sample

Payment Terms: T/T

Supply Ability: 1000 Bag/Bags per Month

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Specifications
Highlight:

MEMS Inertial Measurement Unit

,

Inertial Measurement Unit 10Hz

,

INS inertial navigation system IMU570

Usage:
Position Sensor
Theory:
Capacitance Sensor
Output:
Optional
Product Name:
MEMS Integrated Inertia Navigation System
Interface Type:
Micro-DB9,RS422
Power Supply:
+5±0.5V(DC)
Impact::
100g@11ms,Triaxial (half Sinusoidal)
Vibration::
10~2000Hz,10g
Working Temperature::
-40~85℃
Port:
SHENZHEN
Usage:
Position Sensor
Theory:
Capacitance Sensor
Output:
Optional
Product Name:
MEMS Integrated Inertia Navigation System
Interface Type:
Micro-DB9,RS422
Power Supply:
+5±0.5V(DC)
Impact::
100g@11ms,Triaxial (half Sinusoidal)
Vibration::
10~2000Hz,10g
Working Temperature::
-40~85℃
Port:
SHENZHEN
Description
IMU570 10Hz MEMS Inertial Measurement Unit INS Navigation System

 

Low Price IMU for Navigation Inertial Measurement Unit

 

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:

 

  1. 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.

 

  1. 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.

 
IMU570 10Hz MEMS Inertial Measurement Unit INS Navigation System 2

 

 

 

 

 

The installation of IMU570 should match the axis of the coordinate system, otherwise the angular velocity data measured are inaccurate. Following Right Hand Rule Principle 1, the axis of the coordinate system can be quickly allocated and determined. Stretch out your right hand and expand your thumb, index finger and middle finger. The direction of thumb finger is X-axis positive; the direction of index finger is Y-axis positive, and the direction of middle finger is Z-axis positive.

 

Right Hand Rule Principle 2

IMU570 three DOF gyroscope can measure angular velocity in three directions. Following Right Hand Rule Principle 2, the angular velocity direction of axially rotating coordinate axes can be determined quickly. The right hand grasps the rotation axis and extends the thumb. The direction of the thumb finger is the positive direction of the axis, while the direction of the other four fingers bending is the positive direction of the angular velocity on the axis. On the contrary, the right hand grasps the rotation axis and extends the thumb. The direction of the thumb finger is the negative direction of the axis, and the direction of the other four fingers bending is the angle of the axis. Velocity is negative.


Dimension 

 

IMU570 10Hz MEMS Inertial Measurement Unit INS Navigation System 4
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