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Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System

    Buy cheap Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System from wholesalers
     
    Buy cheap Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System from wholesalers
    • Buy cheap Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System from wholesalers

    Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System

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    Brand Name : NAVI OPTICS
    Model Number : DINS-100
    Certification : CCS
    Payment Terms : T/T
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    Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System

    Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System


    Introduction

    DINS 100 dual-axis rotary laser gyro inertial navigation system is a high-performance inertial navigation and measurement equipment, which adopts 90-type two-frequency machine shaking laser gyroscope and quartz flexure accelerometer, and the performance of the system has been significantly improved through high-precision error calibration, temperature compensation technology, and dual-axis rotary on-line autonomous calibration and error self-compensation technology. The system adopts electromagnetic shielding design, thermal balance design, vibration modal design, sealing design and strict manufacturing process to ensure excellent environmental adaptability.


    Features

    High precision 90 type 2-frequency machine shake laser gyroscope

    Dual-axis rotational self-calibration and error self-compensation

    Static base and moving base initial alignment

    Error parameter calibration and compensation in full temperature range

    Preset GNSS/odometer/trip-meter interface

    Can be configured to different navigation modes

    Excellent environmental adaptability

    Military standard


    Application

    Ship navigation

    Underwater submarine navigation

    Positioning and Orientation of Missile Launch Vehicles

    High-precision Attitude Measurement



    Performance
    Start-up time6h
    Pure Inertial Position2nm/10d, peak
    Pure Inertial Velocity0.5m/s, 1σ
    Pure Inertial Attitude0.005deg, 1σ
    Pure Inertial Heading0.008×sec(Lat) deg, 1σ
    Heave5cm or 5%
    Measuring Range
    Angular Velocity±400deg/s
    Acceleration±20g
    Working Environment
    Working Temperature-40℃~+55℃
    Storage Temperature-55℃~+70℃
    Vibration0.04g2/hz@ 20~2000hz
    Normal Operation/30g @ 6ms/50g @ 11 ms

    no damage under shock
    Electrical Characteristics
    Operating Voltage28VDC
    Power Consumption≤200W
    Communication InterfaceRS422/RS232/CAN/Ethernet
    Physical Characteristics
    Dimensions (W x D x H)φ550×500 mm
    Weight≤60kg


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