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Merak-A03 GNSS Strapdown Aircraft Inertial Navigation System FOG INS
Merak-A03 GNSS Strapdown Aircraft Inertial Navigation System FOG INS
Specifications
Brand Name :
Star & Inertia Technology
Model Number :
Merak-A03
Place of Origin :
China
MOQ :
1 set
Supply Ability :
500 sets per year
Delivery Time :
30 work days
Payment Terms :
T/T
Price :
$1000-$100000
Alignment time :
≤5min
Position accuracy/Pure inertia :
≤4nm/1h,CEP
Position accuracy/INS/GNSS combination :
better than GNSS
Speed ​​accuracy/Pure inertia :
≤3.0m/s,RMS
Speed ​​accuracy/INS/GNSS combination :
≤0.2m/s,RMS
Heading Accuracy/Pure inertia :
≤0.2°sec(L),RMS
Heading Accuracy/INS/GNSS combination :
≤0.1°,RMS
Pitch & Roll Accuracy/Pure inertia :
≤0.05°,RMS
Pitch & Roll Accuracy/INS/GNSS combination :
≤0.03°,RMS
Dimensions :
110×110×100mm
Weight :
＜1.7kg
Temperature :
-40℃~60℃
Input Voltage :
DC24V(±25%)
Description

Aerospace FOG INS(Merak-A03)


Delivering exceptional navigation performance, this optical INS employs FOG/RLG gyros and quartz accelerometers in strapdown configuration. The real-time fusion center combines inertial data with GNSS, celestial and other sources.


Key advantages for UAV applications:

1) Reliable ground/air alignment;

2) Multiple alignment mode selection;

3) Scalable navigation augmentation;

4) Continuous system monitoring.

Series Aerospace Inertial Navigation System(INS-A)
Type Merak-A03
Accelerometer Months Bias Repeatability(1σ) ≤50μg
Months Scale Factor Accuracy(1σ) ≤50ppm
Gyro Bias Repeatability(1σ) ≤0.02°/hr
Scale Factor Accuracy(1σ) ≤50ppm
Random walk(1σ) ≤0.01°/√hr
Features Position Accuracy Pure inertia ≤4nm/1h,CEP
INS/GNSS combination better than GNSS
Speed Accuracy Pure inertia ≤3.0m/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 ≤0.2°sec(L),RMS
INS/GNSS combination ≤0.1°,RMS
Pitch & Roll Accuracy Pure inertia ≤0.05°,RMS
INS/GNSS combination ≤0.03°,RMS
Characteristics Power consumption ＜15W
Dimensions 110×110×100
Weight ＜1.7kg
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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Merak-A03 GNSS Strapdown Aircraft Inertial Navigation System FOG INS

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Product Detail
Brand Name :
Star & Inertia Technology
Model Number :
Merak-A03
Place of Origin :
China
MOQ :
1 set
Supply Ability :
500 sets per year
Delivery Time :
30 work days
Contact Supplier
Merak-A03 GNSS Strapdown Aircraft Inertial Navigation System FOG INS

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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