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Aviation Navigation TDF645B Airborne Optical Gyro Inertial Navigation

    Buy cheap Aviation Navigation TDF645B Airborne Optical Gyro Inertial Navigation from wholesalers
     
    Buy cheap Aviation Navigation TDF645B Airborne Optical Gyro Inertial Navigation from wholesalers
    • Buy cheap Aviation Navigation TDF645B Airborne Optical Gyro Inertial Navigation from wholesalers

    Aviation Navigation TDF645B Airborne Optical Gyro Inertial Navigation

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    Brand Name : NAVI OPTICS
    Model Number : TDF645B
    Certification : CCS
    Payment Terms : L/C,T/T
    Supply Ability : 10 sets per month
    Delivery Time : 5-8 work days
    • Product Details
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    Aviation Navigation TDF645B Airborne Optical Gyro Inertial Navigation

    Aviation Navigation TDF645B Airborne Optical Gyro Inertial Navigation


    1 Introductin

    The Airborne Optical Gyro Inertial Navigation System (INS) employs optical gyroscopes and quartz accelerometers as its core sensing components, utilizing either a strapdown or dithered (modulated) system architecture. Operating with advanced navigation software at high processing speeds, the system delivers real-time navigation data through its sophisticated computational core.This product series features multi-source integration capabilities, supporting fusion of satellite navigation, celestial navigation, radio navigation, altimeter data, and visual navigation systems according to mission requirements. Offering flexible operational modes ranging from pure inertial navigation to optimized multi-sensor fusion, it provides comprehensive navigation parameters including precise position, velocity, and attitude information for airborne platforms.


    2 Application Fields

    Suitable for fixed-wing UAVs, rotary-wing UAVs, and specialized airborne vehicles.


    3 Performance Characteristics

    Supports multi-sensor fusion, incorporating satellite, celestial, altimeter, radio, and visual navigation data.

    Supports switching between self-alignment, moving-base alignment, and transfer alignment based on customer needs.

    Capable of alignment on ground-based vibrating platforms and in-flight alignment.

    Equipped with system fault detection and alarm functions.


    4 Main parameters


    TypeTDF645B
    AccelerometerMonths Bias Repeatability≤20μg
    Months Scale Factor Accuracy≤20ppm
    GyroBias Repeatability≤0.008°/hr
    Scale Factor Accuracy≤20ppm
    Random walk≤0.003°/√hr
    FeaturesPosition accuracyPure inertia≤1nm/6h
    Inertial navigation satellite combinationbetter than satellite accuracy
    Velocity accuracyPure inertia≤1.0m/s
    Inertial navigation satellite combination≤0.2m/s
    Angular Rate≥±400°/sec
    Angular Acceleration100000°/sec2
    Acceleration>25g
    Angular AttitudeAny Orientation
    Alignment time≤8min
    Input/output3 RS422 full-duplex serial ports, 1 100M Ethernet port
    Alignment TimeTime<15min
    AHRS Applications PerformanceHeading AccuracyPure inertia≤0.1°sec(L)
    Satellite navigation combination≤0.05°sec(L)
    Pitch & Roll AccuracyPure inertia≤0.05°
    Satellite navigation combination≤0.02°
    CharacteristicsPower consumption<40W
    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
    MTBF>15000 hours


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