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GPS-Enabled MEMS Inertial Navigation System for Land Vehicle ±16g Accelerometer Range and Acc Zero Bias Stability of 0.2mg

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap GPS-Enabled MEMS Inertial Navigation System for Land Vehicle ±16g Accelerometer Range and Acc Zero Bias Stability of 0.2mg from wholesalers
     
    Buy cheap GPS-Enabled MEMS Inertial Navigation System for Land Vehicle ±16g Accelerometer Range and Acc Zero Bias Stability of 0.2mg from wholesalers
    • Buy cheap GPS-Enabled MEMS Inertial Navigation System for Land Vehicle ±16g Accelerometer Range and Acc Zero Bias Stability of 0.2mg from wholesalers

    GPS-Enabled MEMS Inertial Navigation System for Land Vehicle ±16g Accelerometer Range and Acc Zero Bias Stability of 0.2mg

    Ask Lasest Price
    Brand Name : FIREPOWER
    Model Number : INS100E
    Certification : CE
    Price : 2000$
    Payment Terms : L/C,D/P,T/T,Western Union
    Supply Ability : 1 week for sample
    Delivery Time : 1 week
    • Product Details
    • Company Profile

    GPS-Enabled MEMS Inertial Navigation System for Land Vehicle ±16g Accelerometer Range and Acc Zero Bias Stability of 0.2mg

    Low Cost MEMS lnertial Navigation System with GPS for Land Vehicle

    • Product Description

    INS100E integrated navigation system (hereinafter referred to as integrated navigation system) has built-in high-performance MEMS gyroscope and accelerometer, which can receive internal GNSS data, realize multi-sensor fusion and integrated navigation solution algorithm, and have short-term inertial navigation capability when GNSS is invalid.The product has high reliability and strong environmental adaptability. By matching different software, the product can be widely used in the fields of industry unmanned motion carrier, unmanned vehicle, unmanned ship, communication in motion, mapping, stable platform and so on.


    • System function

    The integrated navigation system can carry out integrated navigation by using the satellite navigation information received internally, and output the pitch, roll, heading, position, speed, time and other information of the carrier; After losing the satellite signal, it outputs the position, velocity and attitude information of inertial solution, and has a certain navigation accuracy maintenance function in a short time.

    • Product Parameter

    Project

    Metrics (RMS)

    Remark

    Heading accuracy

    GNSS valid ①

    0.1°

    Heading holding

    0.2°/min

    GNSS failure

    Attitude accuracy

    GNSS is valid

    0.1°

    Single-point L1/L2, RTK

    Attitude holding

    0.2°/min

    GNSS failure

    Positioning accuracy

    Horizontal, GNSS valid; RTK

    1.5m;1cm+1ppm

    Single point L1/L2; Differential

    Elevation, GNSS valid; RTK

    2.5m;2cm+1ppm

    Single point L1/L2; Differential

    Position holding, GNSS failure

    20m

    Unlocked for 60s

    Horizontal velocity accuracy

    GNSS is valid

    0.1m/s

    Single-point L1/L2,RTK

    Gyroscope

    Measuring range

    ±500°/s

    Zero bias stability

    4°/h

    Allan variance

    Accelerometer

    Measuring range

    ±16g

    Customizable 200 g

    Zero bias stability

    0.2mg

    Allan variance

    Satellite board

    Cold start

    < 30 seconds

    Open environment

    Hot start

    5 seconds

    Open environment

    Type of receiver

    BDS B1I/B2I/B3I

    GPS L1C/A/L2P (Y)/L2C/L5

    GLONASS G1/G2

    Galileo E1/E5a/E5b

    QZSS L1/L2/L5

    Communication interface

    RS232

    Route 2

    RS422

    Route 1

    Electrical characteristics

    Voltage

    9~36VDC

    Power consumption

    ≤3W

    Ripple

    100 mV

    P-P

    Structural characteristics

    Size

    80 mm×53 mm×23mm

    Weight

    ≤150g

    Use environment

    Operating temperature

    -40℃~+60℃

    Storage temperature

    -45℃~+65℃

    Vibration

    20~2000Hz,6.06g

    Impact

    30g,11ms

    Degree of protection

    IP65

    Reliability

    MTBF

    30000h

    Life span

    > 15 years

    Continuous working time

    >24h

    ① Effective 2m baseline of dual antenna, or dynamic alignment of single antenna


    • Outline Drawing


    Quality GPS-Enabled MEMS Inertial Navigation System for Land Vehicle ±16g Accelerometer Range and Acc Zero Bias Stability of 0.2mg for sale
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