CSSC Star&Inertia Technology co.,ltd.

CSSC Star&Inertia Technology co.,ltd.

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Merak-A05 Optical Gyroscope Aircraft Inertial Navigation System Drone UAVs 2000Hz

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CSSC Star&Inertia Technology co.,ltd.
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Province/State:hubei
Country/Region:china
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Merak-A05 Optical Gyroscope Aircraft Inertial Navigation System Drone UAVs 2000Hz

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Brand Name :Star & Inertia Technology
Model Number :Merak-A05
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 :≤5min
Position accuracy/Pure inertia :≤2nm/1h,CEP
Position accuracy/INS/GNSS combination :better than GNSS
Speed ​​accuracy/Pure inertia :≤1.5m/s,RMS
Speed ​​accuracy/INS/GNSS combination :≤0.2m/s,RMS
Heading Accuracy/Pure inertia :≤0.1°sec(L),RMS
Heading Accuracy/INS/GNSS combination :≤0.05°,RMS
Pitch & Roll Accuracy/Pure inertia :≤0.03°,RMS
Pitch & Roll Accuracy/INS/GNSS combination :≤0.02°,RMS
Dimensions :130×130×110mm
Weight :<2.2kg
Temperature :-40℃~60℃
Input Voltage :DC24V(±25%)
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Aerospace FOG INS(Merak-A05)


The airborne optical gyro inertial navigation system uses optical gyroscopes and quartz accelerometers as core sensors, employing strapdown or modulation technology systems. It operates advanced navigation software at high speeds internally, calculating and outputting navigation information in real-time. This series of products can integrate navigation information from satellites, astronomy, altimeters, radio, vision, etc., according to user needs, supporting pure inertial and multi-source information fusion working modes, providing users with comprehensive navigation information for the carrier.


Applications: UAVs and special aircraft.


Capabilities:

1) Ground/air alignment;

2) Alignment mode switching;

3) Sensor fusion;

4) Fault detection.

Series Aerospace Inertial Navigation System(INS-A)
Type Merak-A05
Accelerometer Months Bias Repeatability() 30μg
Months Scale Factor Accuracy() 30ppm
Gyro Bias Repeatability() ≤0.01°/hr
Scale Factor Accuracy() 30ppm
Random walk() ≤0.005°/√hr
Features Position Accuracy Pure inertia 2nm/1h,CEP
INS/GNSS combination better than GNSS
Speed Accuracy Pure inertia 1.5m/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 0.1°sec(L),RMS
INS/GNSS combination 0.05°,RMS
Pitch & Roll Accuracy Pure inertia 0.03°,RMS
INS/GNSS combination 0.02°,RMS
Characteristics Power consumption <15W
Dimensions 130×130×110
Weight <2.2kg
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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