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Model XB185D High Accury Single-axis Fiber Optic Gyroscope With 0.05 °/hr Bias Drift

    Buy cheap Model XB185D High Accury Single-axis Fiber Optic Gyroscope With 0.05 °/hr Bias Drift from wholesalers
     
    Buy cheap Model XB185D High Accury Single-axis Fiber Optic Gyroscope With 0.05 °/hr Bias Drift from wholesalers
    • Buy cheap Model XB185D High Accury Single-axis Fiber Optic Gyroscope With 0.05 °/hr Bias Drift from wholesalers

    Model XB185D High Accury Single-axis Fiber Optic Gyroscope With 0.05 °/hr Bias Drift

    Ask Lasest Price
    Supply Ability : 30 set per month
    Delivery Time : 15 Days
    Brand Name : THUNDSEA
    Model Number : XB185D
    Certification : CCS
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    Model XB185D High Accury Single-axis Fiber Optic Gyroscope With 0.05 °/hr Bias Drift

    Model XB185D High Accury Single-axis Fiber Optic Gyroscope With 0.05 °/hr Bias Drift


    1. Product introduction

    1.1 Working Principle and Function
    This product is an inertial angular rate sensor based on the principle of Sagnac effect, which is used to measure the angular rate movement of the carrier around the sensitive axis of this sensor. This unit takes the fiber optic coil as the angular rate sensitive unit and the closed-loop detection circuit as the basis.
    Two beams from a laser are injected into the same fibre but in opposite directions. Due to the Sagnac effect, the beam travelling against the rotation experiences a slightly shorter path delay than the other beam. The resulting differential phase shift is measured through interferometry, thus translating one component of the angular velocity into a shift of the interference pattern which is measured photometrically.
    Beam splitting optics launches light from a laser diode into two waves propagating in the clockwise and anticlockwise directions through a coil consisting of many turns of optical fibre. The strength of the Sagnac effect is dependent on the effective area of the closed optical path: this is not simply the geometric area of the loop but is enhanced by the number of turns in the coil.
    This product is an inertial sensor composed of optical system, corresponding power supply and data processing circuit. It can provide three-axis angle increment information.


    1.2 Configuration

    The product is mainly composed of the following components:

    a) Optical part: light source, coupler, Y modulator, fiber coil, detector;

    b) Circuit part: processor board, light source board and preamplifier;

    c) Structural part: body, cover, etc.1.3 overall installation size and installation method


    1.3 Overall dimensions

    Single gyroscope configuration: 98mm×98mm×34mm



    1.3.1 Iinstallation method

    The gyro is fixed with 4 M5 screws and metal support.


    1.4 Weight


    WeightNote
    480g±20gThe weight of the product includes the cables,
    connectors and other accessories attached to the
    gyroscope


    1.5 Technical parameters

    Parameter nameNOTE
    Scale factor asymmetry
    (ppm)
    ≤50≤50
    Scale factor nonlinearity(ppm)≤50≤50
    Scale factor Repeatability at full
    temperature range from ﹣40℃ till 60℃
    (ppm,1σ)
    ≤50≤50
    Temperature scale factor polar deviation
    (ppm)
    ≤100≤200After the compensation
    Absolute value of zero deviation
    (°/h)
    ≤10≤10Deduction to speed
    Bias Drift at fixed temperature
    (°/h,10s,1σ)
    ≤0.05≤0.05Constant temperature at a fixed point in the total
    temperature range
    Zero bias repeatability(°/h,1σ)≤0.05≤0.05Constant temperature at a fixed point in the total
    temperature range
    Zero bias temperature sensitivity
    (°/h/℃)
    ≤0.01≤0.01The total temperature range
    Zero bias sensitivity
    (°/h/Gs)
    ≤0.02≤0.02
    Warm up time
    (min)
    ≤1≤3The time from power on to the gyro output
    performance meeting the target requirements
    Range of measured angular rate
    (°/s)
    ≥±400≥±260
    The threshoid value
    (°/h)
    ≤0.05≤0.05
    Resolution
    (°/h)
    ≤0.05≤0.05
    Random Walk
    (°/h½)
    ≤0.01≤0.01
    Input shaft misalignment Angle
    (')
    ≤60≤60
    Misalignment Angle is not repeatable
    (",1σ)
    ≤20≤20Constant temperature test
    Bandwidth
    (Hz)
    ≥200≥200
    Output delay time
    (μs)
    ≤500≤500
    The random vibration is zero deviation
    (°/h)
    ≤0.1≤0.1
    Zero deciation before and after impact
    (°/h)
    ≤0.1≤0.1
    Parameter stabilization time
    (month)
    ≥18≥18

    1.6 Mechanical and electrical interfaces


    1.6.1 Mechanical interface

    Product shell bottom as the cutting Angle square, cutting Angle of the square corners of uniform four Φ 5.2 installation
    hole, hole spacing (80 ± 0.1 mm) x (80 ± 0.1 mm); The bottom surface of the shell is the mounting plane of the gyro, the
    flatness is 0.01.


    1.6.2 Electrical interface

    XB185D gyro signal output connector adopts J30-21TJ socket of guihang electric appliance (corresponding acquisition

    line is J30-21ZK). Socket pin signal definition:

    Pin numberSignal namePhysical meaning
    1,12The main board +5VGyro motherboaed power supply
    13,14The main board ±5V(Ground wire)
    4,15The main board -5V
    6,16The light source +5V(Ground wire)Gyro power supply
    7,17The light source +5V
    2(Reserved external synchronization
    signal)
    TTL level(reserved)
    3,5NCStandby
    8,18T+RS422 hair
    9,19T-
    10,20R+RS422 receiver(differential synchronous
    signal)
    11,21R-

    Model XB185D High Accury Single-axis Fiber Optic Gyroscope With 0.05 °/hr Bias DriftModel XB185D High Accury Single-axis Fiber Optic Gyroscope With 0.05 °/hr Bias Drift

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