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GNSS Inertial Navigation Guidance Attitude Measurement System for Uav Navigation Gyroscope

    Buy cheap GNSS Inertial Navigation Guidance Attitude Measurement System for Uav Navigation Gyroscope from wholesalers
     
    Buy cheap GNSS Inertial Navigation Guidance Attitude Measurement System for Uav Navigation Gyroscope from wholesalers
    • Buy cheap GNSS Inertial Navigation Guidance Attitude Measurement System for Uav Navigation Gyroscope from wholesalers

    GNSS Inertial Navigation Guidance Attitude Measurement System for Uav Navigation Gyroscope

    Ask Lasest Price
    Brand Name : FIREPOWER
    Model Number : INS500
    Price : 7000$
    Payment Terms : L/C,T/T,Western Union
    Supply Ability : 500/month
    Delivery Time : 1 week for sample
    • Product Details
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    GNSS Inertial Navigation Guidance Attitude Measurement System for Uav Navigation Gyroscope

    Product Description


    INS500 fiber-optic integrated navigation system (hereinafter referred to as "inertial navigation") is based on high-precision closed-loop fiber-optic gyroscope, accelerometer and high-end GNSS receiving board, and is realized through multi-sensor fusion and navigation calculation algorithm. It provides high-precision attitude, speed, position and other information to meet the requirements of high-precision measurement and control. Its main application fields include:
    Reference Inertial Navigation System of Large Unmanned Moving Carrier
    Marine compass
    On-board positioning and orientation
    High-precision mobile measurement
    High precision stable platform


    Technical Parameters


    Project

    Test conditions

    INS500A indicator

    INS500B indicator

    Positioning

    Precision

    GNSS Valid, Single Point

    1.2m(RMS)

    1.2m(RMS)

    GNSS Valid, RTK

    2cm+1ppm(RMS)

    2cm+1ppm(RMS)

    Position hold (GNSS failure)

    1.5nm/h(50%CEP),

    5nm/2h(50%CEP)

    0.8nm/h(CEP),

    3.0nm/3h(CEP)

    Heading

    Precision

    Self-seeking north

    0.1 ° × sec (Lati), Lati is latitude (RMS), 10 min

    0.06 ° × sec (Lati), 5min alignment of stationary base;

    0.03 ° × sec (Lati), 10 min alignment of stationary base;

    Where Lati denotes the latitude (RMS).

    Course keeping (GNSS failure)

    0.05°/h(RMS),

    0.1°/2h(RMS)

    0.02°/h(RMS),

    0.05°/3h(RMS)

    Posture

    Precision

    GNSS is valid

    0.03°(RMS)

    0.01°(RMS)

    Attitude hold (GNSS failure)

    0.02°/h(RMS),

    0.06°/2h(RMS)

    0.01°/h(RMS),

    0.03°/3h(RMS)

    Speed

    Precision

    GNSS valid, single point L1/L2

    0.1m/s(RMS)

    0.1m/s(RMS)

    Speed hold (GNSS failure)

    2m/s/h(RMS),

    5m/s/2h(RMS)

    0.8m/s/h(RMS),

    3m/s/3h(RMS)

    Optical fiber

    Gyroscope

    Measuring range

    ±400°/s

    ±400°/s

    Zero bias stability

    ≤0.02°/h

    ≤0.01°/h

    Quartz

    Flexibility

    Accelerate

    Gauge

    Measuring range

    ±20g

    ±20g

    Zero bias stability

    ≤ 50 µg (10 s average)

    ≤ 20 µg (10 s average)

    Communication interface

    RS422

    Route 6

    Baud rate 9.6 kbps ~ 921.6 kbps, default 115.2k bps

    Frequency up to 1000Hz (raw data), default 200Hz

    RS232

    Route 1

    Baud rate 9.6 kbps ~ 921.6 kbps, default 115.2k bps

    Frequency up to 1000Hz (raw data), default 200Hz

    Electrical characteristics

    Voltage

    2436VDC

    Power consumption

    ≤30W

    Structural characteristics

    Size

    199mm×180mm×219.5mm

    Weight

    6.5kg

    ≤ 7.5kg (non-aviation)

    ≤ 6.5kg (optional for aviation)

    Use environment

    Operating temperature

    -40℃~+60℃

    Storage temperature

    -45℃~+65℃

    Vibration (with damping)

    5~2000Hz,6.06g

    Shock (with shock absorption)

    30g,11ms

    Reliability

    Life span

    > 15 years

    Continuous working time

    >24h

    Outline Drawing


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