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High Precise Inertial Navigation System GPS Inertial Navigation Sensor

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap High Precise Inertial Navigation System GPS Inertial Navigation Sensor from wholesalers
     
    Buy cheap High Precise Inertial Navigation System GPS Inertial Navigation Sensor from wholesalers
    • Buy cheap High Precise Inertial Navigation System GPS Inertial Navigation Sensor from wholesalers

    High Precise Inertial Navigation System GPS Inertial Navigation Sensor

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    Model Number : INS500
    Payment Terms : T/T
    Supply Ability : 100/MONTH
    Delivery Time : 15 days for sample
    Brand Name : Firepower
    Certification : CE ROHS
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    High Precise Inertial Navigation System GPS Inertial Navigation Sensor

    GPS navigation sensor high precise inertial sensor with GPS


    INS500 fiber integrated navigation system (the "ins") by the closed loop based on high precision fiber optic gyro, accelerometer and high-end GNSS receiver boards, navigation through multiple sensor fusion and decoding algorithm, provide high precision navigation position, velocity and position information, such as meet the requirement of high precision measurement and control, and main application fields include: The system has inertial/satellite integrated navigation mode and pure inertial mode.

    When GNSS is invalid, it can enter the pure inertia mode (that is, GPS fusion has never been carried out after power is turned on, if the fusion is lost again, it belongs to the integrated navigation mode). After starting, it has accurate attitude measurement function, can output pitch roll course, and pure inertia can static north search.


    ItemsTest ConditionsA0IndicatorsB0Indicators
    Positioning accuracyGNSSValid, single point1.2m(RMS)1.2m(RMS)
    GNSSValid,RTK2cm+1ppm(RMS)2cm+1ppm(RMS)
    Position holding (GNSS failure)1.5nm/h(50%CEP),5nm/2h(50%CEP)0.8nm/h(CEP),3.0nm/3h(CEP)
    Heading accuracyNorth-seekingit self

    0.1°×sec(Lati),

    *Lati:latitude (RMS),10min

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

    0.03°×sec(Lati),Static base 5min alignment;*Lati:latitude (RMS)

    Course keeping (GNSS failure)0.05°/h(RMS),0.1°/2h(RMS)0.02°/h(RMS),0.05°/3h(RMS)
    Attitude accuracyGNSS Valid0.03°(RMS)0.01°(RMS)
    Attitude holding (GNSS failure)0.02°/h(RMS),0.06°/2h(RMS)0.01°/h(RMS),0.03°/3h(RMS)
    Speed accuracyGNSS Valid, single pointL1/L20.1m/s(RMS)0.1m/s(RMS)
    Speed retention (GNSS failure)2m/s/h(RMS),5m/s/2h(RMS)0.8m/s/h(RMS),3m/s/3h(RMS)
    Fiber optical gyroMeasuring range±400°/s±400°/s
    Bias stability≤0.02°/h≤0.01°/h
    Quartz flexibleaccelerometerMeasuring range±20g±20g
    Bias stability≤50µg(10s Average)≤20µg(10s平均)
    Communication interfaceRS4226waysThe baud rate ranges from 9.6 KBPS to 921.6 KBPS. The default baud rate is 115.2 KBPSThe maximum frequency is 1000Hz(raw data), and the default frequency is 200Hz
    RS2321 wayThe baud rate ranges from 9.6 KBPS to 921.6 KBPS. The default baud rate is 115.2 KBPSThe maximum frequency is 1000Hz(raw data), and the default frequency is 200Hz
    Electrical characteristicsVoltage24~36VDC
    Power consumption≤30W
    Structural characteristicsDimension199mm×180mm×219.5mm
    Weight6.5kg≤7.5kg(non-aviation)≤6.5kg (aviation optional)
    EnvironmentWorking temperature-40℃~+60℃
    Storage temperature-45℃~+65℃
    Vibration (with damping)5~2000Hz,6.06g
    Impact (with shock absorption)30g,11ms
    ReliabilityLifetime>15years
    Continuous working time>24h

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