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

    Buy cheap Dubhe-A6 Optical Gyros Quartz RLG Aircraft Inertial Navigation System INS For Astroinertial from wholesalers
     
    Buy cheap Dubhe-A6 Optical Gyros Quartz RLG Aircraft Inertial Navigation System INS For Astroinertial from wholesalers
    • Buy cheap Dubhe-A6 Optical Gyros Quartz RLG Aircraft Inertial Navigation System INS For Astroinertial from wholesalers

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

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    Brand Name : Star & Inertia Technology
    Model Number : Dubhe-A6
    Price : $1000-$100000
    Payment Terms : T/T
    Supply Ability : 500 sets per year
    Delivery Time : 30 work days
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    Dubhe-A6 Optical Gyros Quartz RLG Aircraft Inertial Navigation System INS For Astroinertial

    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.

    SeriesAerospace Inertial Navigation System(INS-A)
    TypeDubhe-A6
    AccelerometerMonths Bias Repeatability()30μg
    Months Scale Factor Accuracy()30ppm
    GyroBias Repeatability()≤0.008°/hr
    Scale Factor Accuracy()10ppm
    Random walk()≤0.003°/√hr
    FeaturesPosition AccuracyPure inertia1nm/6h,CEP
    INS/GNSS combinationbetter than GNSS
    Speed AccuracyPure inertia1.0 m/s,RMS
    INS/GNSS combination0.2m/s,RMS
    Angular Rate≥±400°/sec
    Angular Acceleration100000°/sec2
    Acceleration>25g
    Angular AttitudeAny Orientation
    Input/output3 RS422 full-duplex serial ports, 1 100M Ethernet port
    Alignment time<15min
    AHRS Applications PerformanceHeading AccuracyPure inertia0.02°sec(L),RMS
    INS/GNSS combination0.01°,RMS
    Pitch & Roll AccuracyPure inertia0.015°,RMS
    INS/GNSS combination0.01°,RMS
    CharacteristicsPower consumption40W
    Dimensions193×169×160
    Weight<6.5kg
    Temperature-40℃~60℃
    Shock15g,Half-sine wave 11ms
    Input VoltageDC24V(±25%)
    coolingConduction to mounting plate
    Vibration20~2000Hz,6.06g
    MTBF10000 hours


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