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Shenzhen Rion Technology Co., Ltd.
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Highly Durable IMU Inertial Measurement Unit for Aerospace Motion Sensing

Product Details

Place of Origin: China

Brand Name: RION

Certification: CE, FCC

Model Number: IMU570

Payment & Shipping Terms

Minimum Order Quantity: 1pcs

Price: US$500

Packaging Details: 1pcs in each inner box , 80pcs in each carton

Delivery Time: 1-2 weeks

Payment Terms: Paypal , T/T bank wire

Supply Ability: 30000pcs per month

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Specifications
Highlight:

Aerospace IMU Inertial Measurement Unit

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Highly Durable IMU Inertial Measurement Unit

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IMU Inertial Measurement Unit

Roll / Tilt 1σ (Dynamic):
0.5°
Measue Range:
1800°/s
Resolution:
≤0.001°/s
Cross-coupling:
≤0.1%
Working Temperature:
-40~85℃
Vibration:
-40°C~+85°C
Impact:
10~2000Hz,10g
Weight:
≤60g (excluding Cables)
Roll / Tilt 1σ (Dynamic):
0.5°
Measue Range:
1800°/s
Resolution:
≤0.001°/s
Cross-coupling:
≤0.1%
Working Temperature:
-40~85℃
Vibration:
-40°C~+85°C
Impact:
10~2000Hz,10g
Weight:
≤60g (excluding Cables)
Description
Highly Durable IMU Inertial Measurement Unit for Aerospace Motion Sensing

Highly Durable IMU Inertial Measurement Unit for Aerospace Motion Sensing

IMU570 INERTIAL NAVIGATION UNIT.pdf

Product Description:

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 / RS485 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.

PRODUCT FEATURES :

1.storage temperature :-40~85℃

2.Vibration:10~2000Hz,10g

3.power supply :+5±0.5V(DC)

4.impact:100g@11ms,3 Axial Direction (Half Sinusoid)

SPECIFICATION:

IMU570

Highly Durable IMU Inertial Measurement Unit for Aerospace Motion Sensing 0
PARAMETERS
Attitude angle Roll / Tilt 1σ (Dynamic) 0.5°
Heading 0.5°
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
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,3 Axial Direction (Half Sinusoid)
Weight ≤60g (excluding cables)

Applications:

★ Autopilot Vehicle

★ Unmanned Aerial Vehicle

★ SOTM attitude unit

★ POS System for Surveying and Mapping

★ High Speed Train Measurement and Control System

★ Ocean and Underwater Surveying and Mapping

★ Flight Control System

 

 

ORDERING INFORMATION:

MODEL DESCRIBE
IMU570-422 RS422 output
IMU570-485 RS485 output

 

 

ELECTRICAL CHARACTERISTICS:

IMU570 The electrical connector type of the integrated inertial navigation system is J30J-15ZKP,the specific PIN definition is shown in the table below;

 

Pin Pin Definition Type Instruction
1 EARTH IN Shell connecting pull end, mobile device connecting power GND, fixed equipment connecting housing protection GND (0V)
2 VDD Power positive Power positive 4.5VDC~7VDC
3 RS422-RX+(RS485-A) IN(OUT) Communication interface(-7V~+12V)
4 RS422-TX-(RS485-B) OUT(OUT) Communication interface(-7V~+12V)
5 RTK-232-GND NC  
6 NC NC  
7 NRST IN External reset function(The descending edge is valid and must be enabled by the manufacturer.)(b)
8 ExtTrig IN External trigger signal(The descending edge is valid and must be enabled by the manufacturer.)(c)
9 GND Power negative Power negative (0V)
10 RS422-GND IN RS422(RS485)communication GND(0V)
11 RS422-RX- IN Communication interface(-7V~+12V)
12 RS422-TX+ OUT Communication interface(-7V~+12V)
13 RTK-RS232-RX NC  
14 RTK-PPS NC  
15 TOV OUT Output Co-frequency Signal(a)
Highly Durable IMU Inertial Measurement Unit for Aerospace Motion Sensing 1Highly Durable IMU Inertial Measurement Unit for Aerospace Motion Sensing 2
Highly Durable IMU Inertial Measurement Unit for Aerospace Motion Sensing 3
 
 
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