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Dubhe-A6 Optical Gyros Quartz RLG Aircraft Inertial Navigation System INS For Astroinertial
Dubhe-A6 Optical Gyros Quartz RLG Aircraft Inertial Navigation System INS For Astroinertial
Specifications
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%)
Description

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

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Product Detail
Brand Name :
Star & Inertia Technology
Model Number :
Dubhe-A6
Place of Origin :
China
MOQ :
1 set
Price :
$1000-$100000
Payment Terms :
T/T
Contact Supplier
Dubhe-A6 Optical Gyros Quartz RLG Aircraft Inertial Navigation System INS For Astroinertial

CSSC Star&Inertia Technology co.,ltd.

Verified Supplier
1 Years
hubei, wuhan
Since 2013
Business Type :
Manufacturer
Main Products :
Laser Inertial Navigation System, Fiber Optic Inertial Navigation System, Aircraft Inertial Navigation System
Total Annual :
5000000-10000000
Employee Number :
300~500
Certification Level :
Verified Supplier
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