High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor

Product Details
Customization: Available
Output Signal Type: Digital Output
Measuring Shaft Quantities: Three
Manufacturer/Factory, Trading Company
Gold Member Since 2023

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Registered Capital
1000000 RMB
Plant Area
1001~2000 square meters
  • High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor
  • High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor
  • High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor
  • High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor
  • High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor
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  • Overview
  • Product Description
  • Main Functions
  • Product Display
  • Product Parameters
  • Product Structure
  • Main Application Fields
  • Company Profile
Overview

Basic Info.

Model NO.
INS500
Accuracy Grade
0.1deg
IP Rating
IP67
Certification
CE
Customized
Customized
Heading Accuracy
0.1deg
Attitude Accuracy
0.03deg
Gyro Range
400°/S
Gyro Zero Bias Stability
≤0.02°/H
Speed Accuracy
0.1m/S
Acc Range
±20g
Accelerometer Zero Bias Stability
≤ 50 µg (10 S Average)
Communication Interface
RS232, RS422
Weight
6.5kg
Vibration
5~2000Hz
Power Consumption
≤30W
Operating Temperature
-40ºC~+60ºC
Transport Package
Sponge and Box
Specification
199mm*180mm*219.5mm
Trademark
AVIC
Origin
China
Production Capacity
500/Month

Product Description

High data output frequency Inertial navigation guidance system with Fiber optic gyro sensor

Product Description

INS500-A0 (B0) fiber-optic integrated navigation system  is based on high-precision closed-loop fiber-optic gyroscope, accelerometer and high-end GNSS receiving board, and is realized through multi-sensor fusion and navigation calculation algorithm. It provides high-precision attitude, speed, position and other information to meet the requirements of high-precision measurement and control. Its main application fields include:
  • Large UAV Reference Inertial Navigation System
  • Marine compass
  • Self-propelled gun orientation
  • Vehicle positioning and orientation
  • High-precision mobile measurement
  • High precision stable platform
The INS500-A0 (B0) optical fiber integrated navigation system is divided into two configurations, INS500-A0 (B0) A0 and INS500-A0 (B0) B0. The electrical, structure and interface are completely the same, but the accuracy is different.

Main Functions

  • The system has inertial/satellite integrated navigation mode and pure inertial mode.
     
  • The inertial navigation system has a built-in GNSS board. When the GNSS is valid, the inertial navigation system can perform integrated navigation with the GNSS, and provide the user with navigation parameters such as the combined position, altitude, speed, attitude, heading, acceleration, and angular velocity, and output information such as the GNSS position, altitude, and speed.
     
  • When the GNSS is invalid, it can enter the pure inertial mode (that is, GPS fusion has never been carried out after power-on, and if it loses lock again after fusion, it belongs to the integrated navigation mode). After starting, it has accurate attitude measurement function, can output the pitch and roll course, and the pure inertia can find the north statically.

Product Display

High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor
High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor

 

Product Parameters

  
Project Test conditions A0 indicator B0 indicator
Positioning accuracy GNSS Valid, Single Point 1.2m(RMS) 1.2m(RMS)
GNSS Valid, RTK 2cm+1ppm(RMS) 2cm+1ppm(RMS)
Position hold (GNSS failure) 1.5nm/h(50%CEP),
5nm/2h(50%CEP)
0.8nm/h(CEP),
3.0nm/3h(CEP)
Heading accuracy Self-seeking north 0.1 ° × sec (Lati), Lati is latitude (RMS), 10 min 0.06 ° × sec (Lati), 5min alignment of stationary base;
0.03 ° × sec (Lati), 10 min alignment of stationary base;
Where Lati denotes the latitude (RMS).
Heading keeping (GNSS failure) 0.05°/h(RMS),
0.1°/2h(RMS)
0.02°/h(RMS),
0.05°/3h(RMS)
Attitude accuracy GNSS is valid 0.03°(RMS) 0.01°(RMS)
Attitude hold (GNSS failure) 0.02°/h(RMS),
0.06°/2h(RMS)
0.01°/h(RMS),
0.03°/3h(RMS)
Speed accuracy GNSS valid, single point L1/L2 0.1m/s(RMS) 0.1m/s(RMS)
Speed hold (GNSS failure) 2m/s/h(RMS),
5m/s/2h(RMS)
0.8m/s/h(RMS),
3m/s/3h(RMS)
Fiber
optical
Gyroscope
Measuring range ±400°/s ±400°/s
Zero bias stability ≤0.02°/h ≤0.01°/h
Quartz flexibility
Accelerometer
Measuring range ±20g ±20g
Zero bias stability ≤ 50 µg (10 s average) ≤ 20 µg (10 s average)
Communication interface RS422 Route 6
Baud rate 9.6 kbps ~ 921.6 kbps, default 115.2k bps
Frequency up to 1000Hz (raw data), default 200Hz
 
RS232 Route 1
Baud rate 9.6 kbps ~ 921.6 kbps, default 115.2k bps
Frequency up to 1000Hz (raw data), default 200Hz
Electrical characteristics Voltage 24~36VDC
Power consumption ≤30W
Structural characteristics Size 199mm×180mm×219.5mm
Weight 6.5kg ≤ 7.5kg (non-aviation)
≤ 6.5kg (optional for aviation)
Use environment Operating temperature -40ºC~+60ºC
Storage temperature -45ºC~+65ºC
Vibration with shock absorption) 5~2000Hz,6.06g
Shock (with shock absorption) 30g,11ms
Reliability Life span > 15 years
Continuous working time >24h

 

Product Structure

High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor

Main Application Fields

High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor
High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor
High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor
 

 

Company Profile


High Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro SensorHigh Data Output Frequency Inertial Navigation Guidance System with Fiber Optic Gyro Sensor



 

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