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Dubhe-A6 – Optical Gyros & Quartz RLG Aircraft Inertial Navigation System (INS) for Astroinertial Applications | Aerospace RLG INS

Dubhe-A6 – Optical Gyros & Quartz RLG Aircraft Inertial Navigation System (INS) for Astroinertial Applications | Aerospace RLG INS

MOQ: 1 set
Price: $1000-$100000
Delivery Period: 30 work days
Payment Method: T/T
Supply Capacity: 500 sets per year
Detail Information
Place of Origin
China
Brand Name
Wuhan Deep Pilot Technology Co.,Ltd.
Model Number
Dubhe-A6
Alignment Time:
≤15min
Position Accuracy/Pure Inertia:
≤1nm/6h,CEP
Position Accuracy/INS/GNSS Combination:
Better Than GNSS
Speed ​​accuracy/Pure Inertia:
≤1.0m/s,RMS
Speed ​​accuracy/INS/GNSS Combination:
≤0.2m/s,RMS
Heading Accuracy/Pure Inertia:
≤0.02°sec(L),RMS
Heading Accuracy/INS/GNSS Combination:
≤0.01°sec(L),RMS
Pitch & Roll Accuracy/Pure Inertia:
≤0.015°,RMS
Pitch & Roll Accuracy/INS/GNSS Combination:
≤0.01°,RMS
Dimensions:
193×169×160mm
Weight:
<6.5kg
Temperature:
-40℃~60℃
Input Voltage:
DC24V(±25%)
Product Description

The Dubhe-A6 is an advanced airborne optical inertial navigation system (INS) designed for UAVs and special aircraft. It integrates precision gyros (FOG/RLG) and quartz accelerometers in strapdown or modulated configurations. The high-speed navigation computer processes real-time data and supports flexible integration of GNSS, celestial, and other navigation sources, delivering accurate and reliable navigation solutions.


Applications

  • Various UAVs

  • Special aircraft

  • Astroinertial navigation platforms


Key Features

  • Robust ground and airborne alignment for precise initialization

  • Configurable alignment methods to suit different mission requirements

  • Multi-sensor fusion capability for enhanced navigation accuracy

  • Comprehensive health monitoring for reliable system operation

 Series Aerospace Inertial Navigation System(INS-A)
Type Dubhe-A6
Accelerometer Months Bias Repeatability() 30μg
Months Scale Factor Accuracy() 30ppm
Gyro Bias Repeatability() ≤0.008°/hr
Scale Factor Accuracy() 10ppm
Random walk() ≤0.003°/√hr
Features Position Accuracy Pure inertia 1nm/6h,CEP
INS/GNSS combination better than GNSS
Speed Accuracy Pure inertia 1.0 m/s,RMS
INS/GNSS combination 0.2m/s,RMS
Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration >25g
Angular Attitude  Any Orientation
Input/output 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time <15min
AHRS Applications Performance Heading Accuracy Pure inertia 0.02°sec(L),RMS
INS/GNSS combination 0.01°,RMS
Pitch & Roll Accuracy Pure inertia 0.015°,RMS
INS/GNSS combination 0.01°,RMS
Characteristics Power consumption 40W
Dimensions 193×169×160
Weight <6.5kg
Temperature  -40℃~60℃
Shock 15g,Half-sine wave 11ms
Input Voltage DC24V(±25%)
cooling Conduction to mounting plate
Vibration  20~2000Hz,6.06g
MTBF 10000 hours


products
PRODUCTS DETAILS
Dubhe-A6 – Optical Gyros & Quartz RLG Aircraft Inertial Navigation System (INS) for Astroinertial Applications | Aerospace RLG INS
MOQ: 1 set
Price: $1000-$100000
Delivery Period: 30 work days
Payment Method: T/T
Supply Capacity: 500 sets per year
Detail Information
Place of Origin
China
Brand Name
Wuhan Deep Pilot Technology Co.,Ltd.
Model Number
Dubhe-A6
Alignment Time:
≤15min
Position Accuracy/Pure Inertia:
≤1nm/6h,CEP
Position Accuracy/INS/GNSS Combination:
Better Than GNSS
Speed ​​accuracy/Pure Inertia:
≤1.0m/s,RMS
Speed ​​accuracy/INS/GNSS Combination:
≤0.2m/s,RMS
Heading Accuracy/Pure Inertia:
≤0.02°sec(L),RMS
Heading Accuracy/INS/GNSS Combination:
≤0.01°sec(L),RMS
Pitch & Roll Accuracy/Pure Inertia:
≤0.015°,RMS
Pitch & Roll Accuracy/INS/GNSS Combination:
≤0.01°,RMS
Dimensions:
193×169×160mm
Weight:
<6.5kg
Temperature:
-40℃~60℃
Input Voltage:
DC24V(±25%)
Minimum Order Quantity:
1 set
Price:
$1000-$100000
Delivery Time:
30 work days
Payment Terms:
T/T
Supply Ability:
500 sets per year
Product Description

The Dubhe-A6 is an advanced airborne optical inertial navigation system (INS) designed for UAVs and special aircraft. It integrates precision gyros (FOG/RLG) and quartz accelerometers in strapdown or modulated configurations. The high-speed navigation computer processes real-time data and supports flexible integration of GNSS, celestial, and other navigation sources, delivering accurate and reliable navigation solutions.


Applications

  • Various UAVs

  • Special aircraft

  • Astroinertial navigation platforms


Key Features

  • Robust ground and airborne alignment for precise initialization

  • Configurable alignment methods to suit different mission requirements

  • Multi-sensor fusion capability for enhanced navigation accuracy

  • Comprehensive health monitoring for reliable system operation

 Series Aerospace Inertial Navigation System(INS-A)
Type Dubhe-A6
Accelerometer Months Bias Repeatability() 30μg
Months Scale Factor Accuracy() 30ppm
Gyro Bias Repeatability() ≤0.008°/hr
Scale Factor Accuracy() 10ppm
Random walk() ≤0.003°/√hr
Features Position Accuracy Pure inertia 1nm/6h,CEP
INS/GNSS combination better than GNSS
Speed Accuracy Pure inertia 1.0 m/s,RMS
INS/GNSS combination 0.2m/s,RMS
Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration >25g
Angular Attitude  Any Orientation
Input/output 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time <15min
AHRS Applications Performance Heading Accuracy Pure inertia 0.02°sec(L),RMS
INS/GNSS combination 0.01°,RMS
Pitch & Roll Accuracy Pure inertia 0.015°,RMS
INS/GNSS combination 0.01°,RMS
Characteristics Power consumption 40W
Dimensions 193×169×160
Weight <6.5kg
Temperature  -40℃~60℃
Shock 15g,Half-sine wave 11ms
Input Voltage DC24V(±25%)
cooling Conduction to mounting plate
Vibration  20~2000Hz,6.06g
MTBF 10000 hours