WUHAN JOHO TECHNOLOGY CO., LTD

Electro-optical Infrared Products Manufacturer

              

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Home ProductsFiber Optic Gyro

Fiber Optic Vertical Gyro Navigation Fiber Optic Vertical Gyroscope system

Fiber Optic Vertical Gyro Navigation Fiber Optic Vertical Gyroscope system

    • Fiber Optic Vertical Gyro Navigation Fiber Optic Vertical Gyroscope system
    • Fiber Optic Vertical Gyro Navigation Fiber Optic Vertical Gyroscope system
    • Fiber Optic Vertical Gyro Navigation Fiber Optic Vertical Gyroscope system
    • Fiber Optic Vertical Gyro Navigation Fiber Optic Vertical Gyroscope system
  • Fiber Optic Vertical Gyro Navigation Fiber Optic Vertical Gyroscope system

    Product Details:

    Place of Origin: CHINA
    Brand Name: JOHO
    Model Number: AINS-20

    Payment & Shipping Terms:

    Minimum Order Quantity: 1set
    Price: Negotation
    Packaging Details: Standard Packing
    Delivery Time: 15days
    Payment Terms: L/C, T/T
    Supply Ability: 100Sets/year
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    Detailed Product Description
    Type: Fiber Optic Vertical Gyro Headig Accuracy(GPS Valid): 0.1deg (Length Of Baseline 2m)
    Attitude (GPS Valid): 0.05deg Position Accuracy (GPS Valid): 3m (Cep) , 2cm+1ppm(Cep) (Post-Differentiation)
    Continuous Working Time: 12h Applications: Aircraft Flight Control And Navigation
    Export Markets: Global Heading: 0~360°

     

    Fiber Optic Vertical Gyro

     

    Navigation Fiber Optic Vertical Gyroscope system

     

    Employing high accuracy FOG, Q-flex accelerometers, dual-frequency GPS position & orientation system, barometric altimeter and advanced integration navigation and attitude measurement algorithm, the performance of Attitude and Azimuth Integrated Navigation Fiber Optic Vertical Gyro has been dramatically improved. Combining built-in high accuracy IMU (inertial measurement unit) with satellite, it could output high accuracy position, speed, attitude, angular speed and acceleration information. While the satellite signal is completely covered, system would enter into pure inertial mode. By use of high accuracy FOG, it could still keep good attitude measurement accuracy in certain time. Integrated with barometric altimeter, it could make correction and get higher accuracy height information.
     


    Application


    Aircraft flight control and navigation
    Ship-borne & vehicle-borne navigation system
    Inertial stability control system
    E-traffic measurement system
    Industrial & agricultural measurement and application



    Technical Specifications

     

    Range
    Heading 0~360°
    Pitch angle ±90°
    Roll angle ±180°
    Angular rate ±300°/s
    Acceleration ±10g
    Positioning & orientation accuracy
    Heading accuracy (GPS valid) 0.1° (length of baseline 2m, 1σ)
    Attitude (GPS valid) 0.05° (1σ)
    Position accuracy (GPS valid) 3m (CEP) , 2cm+1ppm(CEP) (post-differentiation)
    Velocity accuracy (GPS valid) 0.1m/s (rms), (1σ)
    Preparation time
    Start time ≤10s
    Stable time System working normally after GPS and heading valid (specified time depends on surrounding environment, open field 2min)
    Power supply
    Power supply DC12~32V, 24V±10% (rating)
    Power consumption ≤25W
    Reliability
    MTBF 2000h
    Continuous working time ≥12h
    Physical parameters
    System weight ≤3.6kg (excluding antenna and feeder line)
    Physical dimension 191mm×166mm×131.5mm (X, Y, Z)

     

    Contact Details
    Wuhan JOHO Technology Co., Ltd

    Contact Person: Tracey

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