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Dubhe-A6 Optical Gyros Quartz RLG Aircraft Inertial Navigation System INS For Astroinertial

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Dubhe-A6 Optical Gyros Quartz RLG Aircraft Inertial Navigation System INS For Astroinertial

Brand Name : Star & Inertia Technology

Model Number : Dubhe-A6

Place of Origin : China

MOQ : 1 set

Price : $1000-$100000

Payment Terms : T/T

Supply Ability : 500 sets per year

Delivery Time : 30 work days

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%)

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Aerospace RLG INS(Dubhe-A6)


Our advanced airborne optical INS combines precision gyros (FOG/RLG) and quartz accelerometers in strapdown/modulated configurations. The powerful navigation computer processes real-time data with flexible integration of GNSS, celestial, and other navigation sources.


Ideal for various UAVs and special aircraft,

it offers:

1) Robust ground/air alignment;

2) Configurable alignment methods;

3) Multi-sensor fusion capability;

4) Comprehensive health monitoring.

Series Aerospace Inertial Navigation System(INS-A)
Type Dubhe-A6
Accelerometer Months Bias Repeatability(1σ) ≤30μg
Months Scale Factor Accuracy(1σ) ≤30ppm
Gyro Bias Repeatability(1σ) ≤0.008°/hr
Scale Factor Accuracy(1σ) ≤10ppm
Random walk(1σ) ≤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



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