CSSC Star&Inertia Technology co.,ltd.

CSSC Star&Inertia Technology co.,ltd.

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Dubhe-A1 Celestial RLG Inertial Positioning System Inertial Navigation System For Drones

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CSSC Star&Inertia Technology co.,ltd.
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Province/State:hubei
Country/Region:china
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Dubhe-A1 Celestial RLG Inertial Positioning System Inertial Navigation System For Drones

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Brand Name :Star & Inertia Technology
Model Number :Dubhe-A1
Place of Origin :China
MOQ :1 set
Supply Ability :500 sets per year
Delivery Time :30 work days
Price :$1000-$100000
Payment Terms :T/T
Alignment time :≤5min
Position accuracy/Pure inertia :≤1.0nm/1h,CEP
Position accuracy/INS/GNSS combination :better than GNSS
Speed ​​accuracy/Pure inertia :≤1.2m/s,RMS
Speed ​​accuracy/INS/GNSS combination :≤0.2m/s,RMS
Heading Accuracy/Pure inertia :≤0.05°sec(L),RMS
Heading Accuracy/INS/GNSS combination :≤0.03°,RMS
Pitch & Roll Accuracy/Pure inertia :≤0.03°,RMS
Pitch & Roll Accuracy/INS/GNSS combination :≤0.015°,RMS
Dimensions :195×160×108mm
Weight :<3.9kg
Temperature :-40℃~60℃
Input Voltage :DC24V(±25%)
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Aerospace RLG INS(Dubhe-A1)


The airborne optical gyro INS utilizes FOG/RLG gyroscopes and quartz accelerometers as core sensors, adopting strapdown or modulated architecture. Its high-speed navigation computer runs advanced algorithms to provide real-time navigation solutions. The system supports multiple operational modes including pure inertial and multi-source fusion (GNSS, celestial, altimeter, radio, and vision), delivering complete navigation parameters.


Applications include fixed-wing UAVs, rotary-wing UAVs, and special aircraft.

Key features:

1) Ground sway base/airborne alignment capability;

2) Switchable alignment modes (self/transfer/moving base);

3) Multi-source navigation fusion;

4) Fault detection and alarm functions.

Series Aerospace Inertial Navigation System(INS-A)
Type Dubhe-A1
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 1.0nm/1h,CEP
INS/GNSS combination better than GNSS
Speed Accuracy Pure inertia 1.2m/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 5min
AHRS Applications Performance Heading Accuracy Pure inertia 0.05°sec(L),RMS
INS/GNSS combination 0.03°,RMS
Pitch & Roll Accuracy Pure inertia 0.03°,RMS
INS/GNSS combination 0.015°,RMS
Characteristics Power consumption <20W
Dimensions 195×160×108
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


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