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Aviation Navigation TDF61A Airborne Optical Gyro Inertial Navigation

    Buy cheap Aviation Navigation TDF61A Airborne Optical Gyro Inertial Navigation from wholesalers
     
    Buy cheap Aviation Navigation TDF61A Airborne Optical Gyro Inertial Navigation from wholesalers
    • Buy cheap Aviation Navigation TDF61A Airborne Optical Gyro Inertial Navigation from wholesalers

    Aviation Navigation TDF61A Airborne Optical Gyro Inertial Navigation

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    Brand Name : NAVI OPTICS
    Model Number : TDF61A
    Certification : CCS
    Payment Terms : L/C,T/T
    Supply Ability : 10 sets per month
    Delivery Time : 5-8 work days
    • Product Details
    • Company Profile

    Aviation Navigation TDF61A Airborne Optical Gyro Inertial Navigation

    Aviation Navigation TDF61A Airborne Optical Gyro Inertial Navigation


    1 Introduction

    The airborne optical gyro inertial navigation system (INS) employs optical gyros and quartz accelerometers as its core sensing components, operating under either a strapdown or dither-modulated inertial navigation architecture‌. High-speed embedded navigation software processes sensor data in real time to deliver continuous positioning and orientation outputs‌. This product series integrates multi-source navigation inputs including satellite signals (GNSS), celestial observations, barometric altimetry, radio navigation aids, and visual odometry based on mission-specific configurations‌. It offers operational flexibility through selectable modes ranging from standalone inertial navigation to adaptive multi-sensor fusion, delivering comprehensive platform states (position, velocity, attitude) across dynamic environments‌.


    2 Application Fields

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


    3 Performance Characteristics

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

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

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

    Equipped with system fault detection and alarm functions.


    4 Main parameters


    TypeTDF61A
    AccelerometerMonths Bias Repeatability≤50μg
    Months Scale Factor Accuracy≤500ppm
    GyroBias Repeatability≤0.3°/hr
    Scale Factor Accuracy≤500ppm
    Random walk≤0.01°/√hr
    FeaturesPosition accuracyPure inertia≤4nm/1h
    Inertial navigation satellite combinationbetter than satellite accuracy
    Velocity accuracyPure inertia≤3.0m/s
    Inertial navigation satellite combination≤0.2m/s
    Angular Rate≥±400°/sec
    Angular Acceleration100000°/sec2
    Acceleration>25g
    Angular AttitudeAny Orientation
    Alignment time≤5min
    Input/output3 RS422 full-duplex serial ports, 1 100M Ethernet port
    Alignment TimeTime<5min
    AHRS Applications PerformanceHeading AccuracyPure inertia≤0.4°sec(L)
    Satellite navigation combination≤0.2°sec(L)
    Pitch & Roll AccuracyPure inertia≤0.08°
    Satellite navigation combination≤0.03°
    CharacteristicsPower consumption<15W
    Dimensions110×110×100
    Weight<1.7kg
    Temperature-40℃~60℃
    Shock15g,Half-sine wave 11ms
    Input VoltageDC24V(±25%)
    coolingConduction to mounting plate
    Vibration20~2000Hz,6.06g
    MTBF>20000 hours


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