High Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation Technology

Product Details
Customization: Available
Type: Inertial Navigation
Output Signal Type: Digital Output
Manufacturer/Factory, Trading Company
Gold Member Since 2023

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Registered Capital
1000000 RMB
Plant Area
1001~2000 square meters
  • High Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation Technology
  • High Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation Technology
  • High Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation Technology
  • High Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation Technology
  • High Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation Technology
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  • Overview
  • Product Description
  • Product Parameters
  • Product Structure
  • Product Display
  • Main Application Fields
  • Company Profile
Overview

Basic Info.

Model NO.
INS100E
Measuring Shaft Quantities
Three
Accuracy Grade
0.1deg
IP Rating
IP67
Certification
CE
Customized
Customized
Heading Accuracy
0.1deg
Attitude Accuracy
0.1deg (RMS)
Gyro Range
±500°/S
Gyro Zero Bias Stability
4°/H
Horizontal Velocity Accuracy
0.1m/S
Acc Range
±16g
Accelerometer Zero Bias Stability
0.2mg
Communication Interface
RS-422/RS-232
Voltage
9~36V
Mtbf
30000h
Power Consumption
≤3W
Vibration
20~2000Hz
Weight
≤150g
Transport Package
Sponge and Box
Specification
80mm*53mm*23mm
Trademark
AVIC
Origin
China
Production Capacity
500/Month

Product Description

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

Product Description

 

The INS100E 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.

 

Product Parameters

  
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 -40ºC~+60ºC  
Storage temperature -45ºC~+65ºC  
Vibration 20~2000Hz,6.06g  
Impact 30g,11ms  
Degree of protection IP65  
Reliability MTBF 30000h  
Life span > 15 years  
Continuous working time >24h  

Product Structure

  High Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation Technology

Product Display

High Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation Technology



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.

Main Application Fields

High Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation Technology
High Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation Technology
High Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation Technology
 

 

Company Profile


High Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation TechnologyHigh Heading Accuracy Integrated Navigation System with Mems and Satellite Navigation Technology



 

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