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Aviation Navigation TDF41A Airborne Optical Gyro Inertial Navigation

    Buy cheap Aviation Navigation TDF41A Airborne Optical Gyro Inertial Navigation from wholesalers
     
    Buy cheap Aviation Navigation TDF41A Airborne Optical Gyro Inertial Navigation from wholesalers
    • Buy cheap Aviation Navigation TDF41A Airborne Optical Gyro Inertial Navigation from wholesalers

    Aviation Navigation TDF41A Airborne Optical Gyro Inertial Navigation

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    Brand Name : NAVI OPTICS
    Model Number : TDF41A
    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 TDF41A Airborne Optical Gyro Inertial Navigation

    Aviation Navigation TDF41A Airborne Optical Gyro-Inertial Navigation


    1 Introduction

    The airborne optical gyro inertial navigation system (INS) utilizes optical gyros and quartz accelerometers as its core sensors, employing either a strapdown or dithered (modulated) inertial navigation system architecture. It runs advanced navigation software internally at high speed to provide real-time navigation information. This series of products can integrate satellite, celestial, altimeter, radio, and visual navigation information, based on user requirements. It supports multiple operating modes, including purely inertial and multi-sensor fusion, providing users with complete navigation parameters for their platforms.


    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


    TypeTDF41A
    AccelerometerMonths Bias Repeatability≤500μg
    Months Scale Factor Accuracy≤500ppm
    GyroBias Repeatability≤0.1°/hr
    Scale Factor Accuracy≤300ppm
    Random walk≤0.03°/√hr
    FeaturesPosition accuracyPure inertia≤1nm/10min
    Inertial navigation satellite combinationbetter than satellite accuracy
    Velocity accuracyPure inertia——
    Inertial navigation satellite combination≤0.2m/s
    Angular Rate≥±400°/sec
    Angular Acceleration100000°/sec2
    Acceleration>40g
    Angular AttitudeAny Orientation
    Alignment time≤5min
    Input/output2 RS422 serial ports
    Alignment TimeTime<5min
    AHRS Applications PerformanceHeading AccuracyPure inertia——
    Satellite navigation combination≤1°sec(L)
    Pitch & Roll AccuracyPure inertia——
    Satellite navigation combination≤0.2°
    CharacteristicsPower consumption<10W
    Dimensions70×70×53
    Weight<500g
    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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