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High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology

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High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology
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Features
Specifications
Product Name: Integrated Navigation System With Accelerometer
Heading Accuracy: 0.1deg (rms)
Attitude Accuracy: 0.1deg (rms)
Horizontal Velocity Accuracy: 0.1m/s
Gyro Range: ±500°/s
Gyro Zero Bias Stability: 4°/h
Accelerometer Range: ±16g
Accelerometer Zero Bias Stability: 0.2mg
Communication Interface: RS-422/RS-232
Weight: ≤150g
High Light:

High heading accuracy Integrated Navigation System

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Satellite Navigation Integrated Navigation System

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MEMS Integrated Navigation System

Basic Infomation
Place of Origin: CHINA
Brand Name: AVIC
Certification: CE ROHS
Model Number: GI100E-A0-DGI
Payment & Shipping Terms
Packaging Details: sponge+carton
Delivery Time: 10 days
Payment Terms: T/T
Supply Ability: 500/month
Product Description

High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology

 

Product Description

 

The GI100E-A0-DGI integrated navigation system has built-in high-performance MEMS gyroscope and accelerometer, which can receive internal GNSS data, realize multi-sensor fusion and integrated navigation solution algorithm, and have short-term inertial navigation capability when GNSS is invalid.

The product has high reliability and strong environmental adaptability. By matching different software, the products can be widely used in the fields of tactical and industrial unmanned aerial vehicles, unmanned vehicles, unmanned ships, aviation guided bombs, intelligent ammunition, rockets, mobile communication, mapping, seeker and stable platform.

 

Technical indicators

 

Project Metrics (RMS) Remark
Heading accuracy GNSS Valid 0.1°  
Course holding 0.2°/min GNSS failure
Attitude accuracy GNSS is valid 0.1° Single-point L1/L2, RTK
Attitude maintenance 0.2°/min GNSS failure
Positioning accuracy Horizontal, GNSS valid; RTK 1.5m;1cm+1ppm Single point L1/L2; Differential
Elevation, GNSS valid; RTK 2.5m;2cm+1ppm Single point L1/L2; Differential
Position keeping, GNSS failure 20m Unlocked for 60s
Horizontal velocity accuracy GNSS is valid 0.1m/s Single-point L1/L2, RTK
Gyroscope Measuring range ±500°/s  
Zero bias stability 4°/h Allan variance
Accelerometer Measuring range ±16g Customizable 200 G
Zero bias stability 0.2mg Allan variance
Satellite card Cold start < 30 seconds Open environment
Hot start 5 seconds Open environment
Type of receiver BDS B1I/B2I/B3I  
GPS L1C/A/L2P (Y)/L2C/L5
GLONASS G1/G2
Galileo E1/E5a/E5b
QZSS L1/L2/L5
Communication interface RS232 Route 2  
RS422 Route 1  
Electrical characteristics Voltage 9~36VDC  
Power consumption ≤3W  
Ripple 100 mV P-P
Structural characteristics Size 80 mm×53 mm×23mm  
Weight ≤150g  
Use environment Operating temperature -40℃~+60℃  
Storage temperature -45℃~+65℃  
Vibration 20~2000Hz,6.06g  
Impact 30g,11ms  
Degree of protection IP65  
Reliability MTBF 30000h  
Life span > 15 years  
Continuous working time >24h  

 

Main Features

 

The integrated navigation system can carry out integrated navigation by using the satellite navigation information received internally, and output the pitch, roll, course, position, speed, time and other information of the carrier; After losing the satellite signal, it outputs the position, velocity and attitude information of inertial solution, and has a certain navigation accuracy maintenance function in a short time.

 

Product Dimensions

 

High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology 0

 

       L80mm x W53mm x H23mm(L x W x H)

 

High heading accuracy Integrated Navigation System with MEMS and Satellite Navigation Technology 1

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