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Aircraft Laser Inertial Navigation Airborne Optical Gyro Inertial Navigation System with Multi-Source Fusion
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Aircraft Laser Inertial Navigation Airborne Optical Gyro Inertial Navigation System with Multi-Source Fusion
  • name

Aircraft Laser Inertial Navigation Airborne Optical Gyro Inertial Navigation System with Multi-Source Fusion

MOQ: 1 set
Delivery Period: 30 work days
Supply Capacity: 500 sets per year
Details Information
Product Description
Detail Information
Place of Origin
China
Brand Name
Star & Inertia Technology
Model Number
TYL46A
Accelerometer/Months Bias Repeatability（1σ）:
≤20μg
Accelerometer/Months Scale Factor Accuracy（1σ）:
≤20ppm
Gyro/Bias Repeatability（1σ）:
≤0.008°/hr
Gyro/Scale Factor Accuracy（1σ）:
≤20ppm
Gyro/Random Walk（1σ）:
≤0.003°/√hr
Position Accuracy/Pure Inertia:
≤0.8nm/1h
Position Accuracy/Inertial Navigation Satellite Combination:
Better Than Satellite Accuracy
Speed ​​accuracy/Pure Inertia:
≤1.0m/s
Speed ​​accuracy/Inertial Navigation Satellite Combination:
≤0.2m/s
Angular Rate:
≥±400°/sec
Angular Acceleration:
100000°/sec2
Acceleration:
＞25g
Angular Attitude:
Any Orientation
Alignment Time:
≤8min
Input/output:
3 RS422 Full-duplex Serial Ports, 1 100M Ethernet Port
Heading Accuracy/Pure Inertia:
≤0.1°sec(L)
Heading Accuracy/Satellite Navigation Combination:
≤0.05°sec(L)
Pitch & Roll Accuracy/Pure Inertia:
≤0.03°
Pitch & Roll Accuracy/Satellite Navigation Combination:
≤0.015°
Power Consumption:
＜20W
Dimensions:
195×160×108mm
Weight:
＜3.9kg
Temperature:
-40℃~60℃
Shock:
15g，Half-sine Wave 11ms
Input Voltage:
DC24V(±25%)
Cooling:
Conduction To Mounting Plate
Vibration:
20~2000Hz,6.06g
MTBF:
＞20000 Hours
Product Description

Product Description

This airborne optical gyro inertial navigation system (INS) utilizes optical gyroscopes (FOG/RLG) and high-precision quartz accelerometers as core sensors. Employing strapdown or modulation technology, the system operates advanced navigation software at high internal speeds, calculating and outputting navigation data in real-time.

The system supports integration of navigation information from satellites, celestial navigation, altimeters, radio, vision, and other sensors according to user requirements. It can operate in pure inertial mode or multi-source information fusion mode, providing comprehensive, accurate, and reliable navigation information for airborne platforms.

  • Core Sensors: Optical Gyroscopes (FOG/RLG) + Quartz Accelerometers

  • Navigation Modes: Pure inertial navigation and multi-source information fusion

  • Real-Time Data: High-speed internal computation and navigation output

Applications

This high-precision INS is ideal for a variety of airborne applications:

  • Unmanned Aerial Vehicles (UAVs): Reliable attitude, heading, and position reference in GNSS-denied environments

  • Specialized Aircraft & Military Platforms: Accurate navigation under challenging operational conditions

  • Aerospace Navigation Systems: Multi-source fusion supports advanced flight and mission requirements

  • Research & Survey Aircraft: Supports precision measurement and geospatial data collection

  • Integrated Avionics Systems: Seamless integration with satellite, radio, and vision navigation sensors

Advantages

  • Alignment in Challenging Environments: Fast and accurate system initialization in complex conditions

  • Mission-Adaptive Alignment: Flexible alignment strategies for different operational scenarios

  • Enhanced Navigation with Multi-Source Fusion: Integrates multiple navigation sources for higher accuracy and reliability

  • Operational Reliability Assurance: Designed for continuous high-performance operation in airborne platforms

Tags: 

fog inertial navigation system,  

inertial navigation system drone,  

integrated navigation system

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products
PRODUCTS DETAILS
Products

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

AHRS System

IMU Inertial Measurement Unit

Fiber Optic Gyroscope

Ring Laser Gyroscope
Aircraft Laser Inertial Navigation Airborne Optical Gyro Inertial Navigation System with Multi-Source Fusion
  • name
Aircraft Laser Inertial Navigation Airborne Optical Gyro Inertial Navigation System with Multi-Source Fusion
MOQ: 1 set
Delivery Period: 30 work days
Supply Capacity: 500 sets per year
Detail Information
Product Description
Detail Information
Place of Origin
China
Brand Name
Star & Inertia Technology
Model Number
TYL46A
Accelerometer/Months Bias Repeatability（1σ）:
≤20μg
Accelerometer/Months Scale Factor Accuracy（1σ）:
≤20ppm
Gyro/Bias Repeatability（1σ）:
≤0.008°/hr
Gyro/Scale Factor Accuracy（1σ）:
≤20ppm
Gyro/Random Walk（1σ）:
≤0.003°/√hr
Position Accuracy/Pure Inertia:
≤0.8nm/1h
Position Accuracy/Inertial Navigation Satellite Combination:
Better Than Satellite Accuracy
Speed ​​accuracy/Pure Inertia:
≤1.0m/s
Speed ​​accuracy/Inertial Navigation Satellite Combination:
≤0.2m/s
Angular Rate:
≥±400°/sec
Angular Acceleration:
100000°/sec2
Acceleration:
＞25g
Angular Attitude:
Any Orientation
Alignment Time:
≤8min
Input/output:
3 RS422 Full-duplex Serial Ports, 1 100M Ethernet Port
Heading Accuracy/Pure Inertia:
≤0.1°sec(L)
Heading Accuracy/Satellite Navigation Combination:
≤0.05°sec(L)
Pitch & Roll Accuracy/Pure Inertia:
≤0.03°
Pitch & Roll Accuracy/Satellite Navigation Combination:
≤0.015°
Power Consumption:
＜20W
Dimensions:
195×160×108mm
Weight:
＜3.9kg
Temperature:
-40℃~60℃
Shock:
15g，Half-sine Wave 11ms
Input Voltage:
DC24V(±25%)
Cooling:
Conduction To Mounting Plate
Vibration:
20~2000Hz,6.06g
MTBF:
＞20000 Hours
Minimum Order Quantity:
1 set
Delivery Time:
30 work days
Supply Ability:
500 sets per year
Product Description

Product Description

This airborne optical gyro inertial navigation system (INS) utilizes optical gyroscopes (FOG/RLG) and high-precision quartz accelerometers as core sensors. Employing strapdown or modulation technology, the system operates advanced navigation software at high internal speeds, calculating and outputting navigation data in real-time.

The system supports integration of navigation information from satellites, celestial navigation, altimeters, radio, vision, and other sensors according to user requirements. It can operate in pure inertial mode or multi-source information fusion mode, providing comprehensive, accurate, and reliable navigation information for airborne platforms.

  • Core Sensors: Optical Gyroscopes (FOG/RLG) + Quartz Accelerometers

  • Navigation Modes: Pure inertial navigation and multi-source information fusion

  • Real-Time Data: High-speed internal computation and navigation output

Applications

This high-precision INS is ideal for a variety of airborne applications:

  • Unmanned Aerial Vehicles (UAVs): Reliable attitude, heading, and position reference in GNSS-denied environments

  • Specialized Aircraft & Military Platforms: Accurate navigation under challenging operational conditions

  • Aerospace Navigation Systems: Multi-source fusion supports advanced flight and mission requirements

  • Research & Survey Aircraft: Supports precision measurement and geospatial data collection

  • Integrated Avionics Systems: Seamless integration with satellite, radio, and vision navigation sensors

Advantages

  • Alignment in Challenging Environments: Fast and accurate system initialization in complex conditions

  • Mission-Adaptive Alignment: Flexible alignment strategies for different operational scenarios

  • Enhanced Navigation with Multi-Source Fusion: Integrates multiple navigation sources for higher accuracy and reliability

  • Operational Reliability Assurance: Designed for continuous high-performance operation in airborne platforms

Tags: 

fog inertial navigation system,

inertial navigation system drone,

integrated navigation system

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Tel: 8613212796772
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