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CSSC Star&Inertia Technology co.,ltd.
CSSC Star&Inertia Technology co.,ltd.
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Merak-A02 GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL

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Merak-A02 GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL

Brand Name : Star & Inertia Technology

Model Number : Merak-A02

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 : 5m/60s(Ref.),150m/300s(Ref.),CEP

Position accuracy/INS/GNSS combination : better than GNSS

Speed ​​accuracy/Pure inertia : ——

Speed ​​accuracy/INS/GNSS combination : ≤0.2m/s,RMS

Heading Accuracy/Pure inertia : ≤0.5°secL+0.1°/h,RMS

Heading Accuracy/INS/GNSS combination : ≤0.3°,RMS

Pitch & Roll Accuracy/Pure inertia : ≤0.1°,RMS

Pitch & Roll Accuracy/INS/GNSS combination : ≤0.05°,RMS

Dimensions : 100×100×90mm

Weight : <1.35kg

Temperature : -40℃~60℃

Input Voltage : DC24V(±25%)

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Aerospace FOG INS(Merak-A02)


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-A02
Accelerometer Months Bias Repeatability() 100μg
Months Scale Factor Accuracy() 100ppm
Gyro Bias Repeatability() 0.05°/hr
Scale Factor Accuracy() 100ppm
Random walk() 0.02°/hr
Features Position Accuracy Pure inertia 5m/60s(Ref.),150m/300s(Ref.),CEP
INS/GNSS combination better than GNSS
Speed Accuracy Pure inertia ——
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 0.5°secL+0.1°/h,RMS
INS/GNSS combination 0.3°,RMS
Pitch & Roll Accuracy Pure inertia 0.1°,RMS
INS/GNSS combination 0.05°,RMS
Characteristics Power consumption 15W
Dimensions 100×100×90
Weight 1.35kg
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



Product Tags:

aviation inertial guidance system

      

FOG inertial guidance system

      

FOG inertial navigation system aviation

      
China Merak-A02 GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL factory

Merak-A02 GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL Images

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