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Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System from wholesalers
     
    Buy cheap Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System from wholesalers
    • Buy cheap Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System from wholesalers
    • Buy cheap Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System from wholesalers
    • Buy cheap Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System from wholesalers
    • Buy cheap Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System from wholesalers
    • Buy cheap Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System from wholesalers
    • Buy cheap Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System from wholesalers
    • Buy cheap Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System from wholesalers
    • Buy cheap Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System from wholesalers

    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System

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    Brand Name : Firepower
    Model Number : INS100
    Certification : CE
    Price : US$2,000.00~3,000.00
    Payment Terms : T/T
    Supply Ability : 100 pcs per month
    Delivery Time : 2 weeks for sample
    • Product Details
    • Company Profile

    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System

    Product Description
    INS-100 is a high-precision integrated navigation system. It is equipped with three self-developed 40 fiber optic gyroscopes,three-self MEMS accelerometers and GNSS modules, and realizes high-precision positioning and navigation in complex environments through multi-sensor fusion and integrated navigation algorithm. The product has high reliability and strong environmental adaptability. The products can be widely used in intelligent driving, UAV, surveying and mapping, marine compass, stable platform, photoelectric pod, underwater vehicle and other fields.

    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.
    Technical Parameter
    Gyro technology
    Project
    Indicators
    Remark


    Gyro
    Measuring range
    -300°/s ~+300°/s
    Resolution
    ≤0.5°/h
    Bias residual
    -1.0°/h ~+1.0°/h
    Random walk
    0.05 o / h
    Bias stability at room temperature
    ≤0.3°/h(1σ)
    10 seconds smoothing, 1h test result
    Bias stability at full temperature
    ≤0.5°/h(1σ)
    10 seconds smoothing, 1h test result
    Normal-temperature Bias repeatability
    ≤0.3°/h(1σ)
    Statistics of 6 test data
    Bias repeatability at full temperature
    ≤0.5°/h(1σ)
    Take 2 Biasdata at full temperature, high temperature, low temperature and normal temperature respectively
    Scale factor nonlinearity
    ≤200ppm
    Full temperature and constant temperature
    Scale factor repeatability
    ≤200ppm(1σ)
    Full temperature and constant temperature
    Gyro start time
    ≤5s
    Gyro bandwidth
    300Hz
    Design assurance, batch testing
    Installation error residual of three-axis gyroscope
    ≤30"
    Accelerometer technical indicators
    Project
    Indicators
    Remark


    Acceleration
    Measuring range
    -50g ~ +50g
    Design and selection guarantee
    Scale factor nonlinearity
    ≤200ppm
    Design and selection guarantee
    Bias stability at full temperature
    ≤100ug(1σ)
    10 seconds smoothing, 1H test result
    Bias repeatability 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
    Project
    Indicators
    Remark







    Alignment accuracy
    North seeking time
    ≤5min
    Generally, 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 mode
    Optional
    It can realize swaying base alignment, GPS auxiliary alignment during travel, odometer auxiliary alignment during travel and main
    inertial navigation transfer alignment.
    Integrated navigation accuracy (satellite effective)
    Project
    Indicators
    Remark


    Alignment accuracy
    North seeking time
    ≤5min
    Generally, 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 mode
    Optional
    It 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)
    Project
    Indicators
    Remark


    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)
    Details Images
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Outline Drawing
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Factory Photos
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System
    Main Applications
    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System

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    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System

    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System

    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System

    Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System

    Quality Micro-nano Integrated Fiber Optic Gyroscope GNSS/INS Integrated Inertial Navigation System for sale
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