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High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI from wholesalers
     
    Buy cheap High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI from wholesalers
    • Buy cheap High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI from wholesalers

    High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI

    Ask Lasest Price
    Brand Name : AVIC
    Model Number : GI300F-A0-DGI
    Certification : CE ROHS
    Price : negotiable
    Payment Terms : T/T
    Supply Ability : 500/month
    Delivery Time : 10 days
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    High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI

    High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI


    Product Description


    The fiber optic integrated navigation system GI300F-A0-DGI consists of a cost-effective three-axis closed-loop fiber optic gyroscope, accelerometer, and navigation board card. It is implemented through multi-sensor fusion and navigation calculation algorithms, meeting the precise measurement requirements for attitude, heading, and position information in applications such as high-precision mobile measurement systems and medium to large unmanned aerial vehicles.


    Main Function


    • The system has inertial/satellite integrated navigation mode and pure inertial mode.
    • In the inertial/satellite integrated navigation mode, the satellite positioning information received by the internal GNSS receiver can be used for integrated navigation, and the pitch, roll, course, position, speed, time and other information of the carrier can be output; After the signal is lost, the position, velocity and attitude of the inertial solution are output, in which the pitch and roll are required to be kept accurate, with a certain course keeping function in a short time and meter-level positioning accuracy in a short time.
    • After the pure inertial mode (that is, GPS fusion has never been performed after power-on, and if it loses lock again after fusion, it belongs to the integrated navigation mode) is started, it has accurate attitude measurement function, can output the pitch and roll heading, and the pure inertial mode can find the north statically.

    Index Parameter


    ProjectTest conditionsIndicators
    Positioning accuracyGNSS Valid, Single Point1.5m
    GNSS Valid, RT K2cm+1ppm
    Pure inertial horizontal positioning holding80m/5min(CEP)
    500m/10min(CEP)
    1.5nm/30min(CEP)
    Horizontal positioning holding accuracy0.8nm/30min (CEP)
    Heading accuracySingle antenna (RMS)0.1°
    Dual Antenna (RMS)0.2 °/L (L = baseline length) (RMS)
    Course Keeping (RMS)0.2°/30min(RMS),0.5°/h
    Self-north seeking accuracy (RMS)0.2 ° SecL,15 min
    1.0 ° SecL, 5-10 min
    Attitude accuracyGNSS is valid0.02°(RMS)
    Attitude hold (GNSS failure)0.2°/30min(RMS),0.5°/h(RMS)
    Speed accuracyGNSS valid, single point L1/L20.1m/s(RMS)
    GyroscopeMeasuring range±400°/s
    Zero bias stability≤0.3°/h
    AccelerometerMeasuring range±20g
    Zero bias stability≤100µg
    Physical dimensions and electrical characteristicsVoltage9-36V DC
    Power consumption≤ 12W (steady state)
    Interface2 RS 232,1-RS 422,1- PPS
    Dimension/L*W*H/mm92.0 *92.0*90.0
    Weight≤1.0kg
    Environmental characteristicsOperating temperature-40℃~+60℃
    Storage temperature-45℃~+70℃
    Vibration5 ~ 2000Hz, 6.06 G
    Impact30g, 11 ms (with shock)
    Life span> 15 years
    Continuons operating hours> 24 hours

    Dimensions


    L92.0mm x W92.0 mm x H90.0mm(L x W x H)


    High Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGIHigh Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGIHigh Accuracy Inertial Navigation System Three-Axis MEMS Gyro GI300F-A0-DGI

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