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Tactical Grade High-Accuracy GNSS Inertial Navigation System For Vessel Tracking

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap Tactical Grade High-Accuracy GNSS Inertial Navigation System For Vessel Tracking from wholesalers
     
    Buy cheap Tactical Grade High-Accuracy GNSS Inertial Navigation System For Vessel Tracking from wholesalers
    • Buy cheap Tactical Grade High-Accuracy GNSS Inertial Navigation System For Vessel Tracking from wholesalers
    • Buy cheap Tactical Grade High-Accuracy GNSS Inertial Navigation System For Vessel Tracking from wholesalers

    Tactical Grade High-Accuracy GNSS Inertial Navigation System For Vessel Tracking

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    Brand Name : Firepower
    Model Number : INS100
    Certification : CE
    Price : negotiable
    Payment Terms : L/C,T/T
    Supply Ability : 100/Month
    Delivery Time : 2 week for sample
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    Tactical Grade High-Accuracy GNSS Inertial Navigation System For Vessel Tracking

    Tactical Grade High-Accuracy GNSS Inertial Navigation System for Vessel Tracking



    Product Description


    INS-100 is a high-precision integrated navigation system designed for demanding applications requiring exceptional accuracy and reliability. It is equipped with three self-developed 40-grade fiber optic gyroscopes, tthree-self MEMS accelerometers, and advanced GNSS modules. By leveraging multi-sensor fusion and sophisticated integrated navigation algorithms, the system delivers precise positioning and navigation even in complex and dynamic environments.
    With its high reliability and strong environmental adaptability, the INS-100 is suitable for a wide range of applications, including autonomous driving, unmanned aerial vehicles (UAVs), geospatial surveying and mapping, marine compasses, stabilized platforms, electro-optical pods, and underwater vehicles. Its robust design ensures stable and accurate performance across diverse operational conditions, making it an ideal choice for industries requiring superior navigation and motion-sensing capabilities.


    Main functions of the integrated navigation system are as follows:

    1. The initial alignment function is completed by using the output of the inertial device, and the shaking base alignment and the moving alignment can be carried out;
    2. The GPS information received from outside can be used to complete the integrated navigation function and output information such as angle, speed and position.
    3. After the satellite signal is lost, the inertial device output and the odometer input can be used to continue the navigation calculation;
    4. It can output high performance and high sampling rate gyro raw output and add raw data for stable platform control.
    5. The program and configuration parameters can be upgraded online through the serial port.

    Main Parameters



    Gyro technology


    ProjectIndicatorsRemark



    Gyro
    Measuring range-300°/s ~+300°/s
    Resolution≤0.5°/h
    Bias residual-1.0°/h ~+1.0°/h
    Random walk0.05 o / h
    Biasstability at room temperature≤0.3°/h(1σ)10 seconds smoothing, 1H test result
    Biasstability at full temperature≤0.5°/h(1σ)10 seconds smoothing, 1H test result
    Normal-temperature Biasrepeatability≤0.3°/h(1σ)Statistics of 6 test data
    Biasrepeatability at full temperature≤0.5°/h(1σ)Take 2 Biasdata at full temperature, high temperature, low temperature and normal temperature respectively
    Scale factor nonlinearity≤200ppmFull temperature and constant temperature
    Scale factor repeatability≤200ppm(1σ)Full temperature and constant temperature
    Gyro start time≤5s
    Gyro bandwidth300HzDesign assurance, batch testing
    Installation error residual of three-axis gyroscope≤30"

    Accelerometer technical indicators


    ProjectIndicatorsRemark


    Acceleration
    Measuring range-50g ~ +50gDesign and selection guarantee
    Scale factor nonlinearity≤200ppmDesign and selection guarantee
    Biasstability at full temperature≤100ug(1σ)10 seconds smoothing, 1H test result
    Biasrepeatability at full temperature≤100ug(1σ)Take 2 Biasdata at full temperature, high temperature, low temperature and normal temperature respectively
    Scale factor repeatability≤100ppm(1σ)Design and selection guarantee
    Random walk≤0.02m/s/h1/2
    Add up the starting time≤5s
    Triaxial addition installation error residual≤30"

    Alignment accuracy


    Integrated navigation accuracy (satellite effective)

    ProjectIndicatorsRemark



    Alignment accuracy
    North seeking time≤5minGenerally, the standard is 3min or 5min.
    Heading Angle Alignment Repeatability≤1°/cosL
    Pitch Alignment Repeatability≤0.05°
    Roll Angle Alignment Repeatability≤0.05°
    North-seeking modeOptionalIt can realize swaying base alignment, GPS auxiliary alignment during travel, odometer auxiliary alignment during travel and main inertial navigation transfer alignment.

    Inertial navigation accuracy (invalid satellite)


    ProjectIndicatorsRemark



    Inertial navigation accuracy
    Accuracy of course angle maintenance≤2°/h
    Pitch Angle Holding Accuracy≤0.2°/h
    Accuracy of roll angle maintenance≤0.2°/h
    Pure inertial positioning accuracy≤20m(100s)CEP, without external information assistance
    Position positioning accuracy of odometer integrated navigation≤ 0.2% (mileage greater than 3 km)
    Position positioning accuracy of odometer integrated navigation≤1m(50s)

    Size


    Main Application Fields


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