Er Gnssmins 05 Cost Efficient Gnss Aided Mems Ins.

Cost-efficient GNSS aided MEMS INS

ER-GNSS/MINS-05:
1. Delivers accurate navigation information: attitude accuracy: 0.1° (0.03° post-processing), heading accuracy: 0.1° (0.05° post-processing).
2. Built-in full-band full-system dual-antenna positioning and orientation GNSS module.
3. Variety of data interface, support RS422/RS232 and CAN.

Cost-efficient GNSS aided MEMS INS

Er Gnssmins 05 Cost Efficient Gnss Aided Mems Ins.

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    Introduction

    Introduction

    ER-GNSS/MINS-05 is a Cost-efficient GNSS aided MEMS INS with a highly reliable MEMS inertial measurement unit and a dual-antenna full-system full-band positioning and directional satellite module. The integrated navigation fusion algorithm can provide continuous, accurate and reliable positioning, attitude and speed information. It has a variety of communication interfaces and provides standardized user communication protocols, which can meet the aviation, land, Marine and other applications.

     

    Features

    • High reliability and low cost MEMS gyroscope (zero bias instability <2°/h) and MEMS accelerometer (zero bias instability <25μg). The working temperature is -40℃~+80℃, and the temperature compensation of the gyroscope and accelerometer is carried out in the working temperature range, which has better zero bias performance.
    • Built-in full-band full-system dual-antenna positioning and orientation GNSS module, supporting single-antenna high-precision positioning and velocity measurement, supporting dual-antenna fast orientation function.
    • The system can provide accurate integrated navigation information, attitude up to 0.1°, post-processing 0.03°, heading 0.1°, post-processing 0.05°.
    • Variety of data interface, more easy to install and use, support RS422/RS232 and CAN.
    • Precision aluminum alloy shell, high reliability, can be widely used in land, aviation, navigation

    Application areas

    UAV, flight recorder, intelligent unmanned vehicle,

    Roadbed positioning and orientation, channel detection,

    Unmanned surface vehicle, underwater vehicle.

     

    Specifications

    1. system parameter

    ER-GNSS/MINS-05
    Roll & Pitch Accuracy 0.1°
    0.03°(Post Processing)
    Heading 0.1° Dual Antenna GNSS(baseline 1m)
    0.05°(Post Processing)
    Speed accuracy 0.03m/s
    Supply Voltage 6~12V
    Supply Consumption 4W
    Interface 1Way-RS422 or 1Way-RS232 and 1Way-CAN
    Vibration 6.06g
    Shock 5000g,0.1ms
    Operate Temp -40℃~+80℃
    Storage Temp -55℃~+95℃
    Weight <240g
    Size 65mm*70mm*45.5mm

     

    2. Sensor parameter

    Gyro Performance
    Item Parameter Unit
    Range ±450 deg/s
    Bandwidth ≥150 Hz
    Bias stability (1σ) ≤8 deg/hr
    Bias Instability (1σ) ≤2 deg/hr
    Angular Random Walk ≤0.15 °/ √h
    Scale Factor Non-Linearity ≤50 ppm
    Bias Run-Run (1σ) ≤8 deg/hr

     

    Accelerometer Performance
    Item Parameter Unit
    Range ±15 g
    Bandwidth ≥150 Hz
    Bias stability (1σ) 0.1 mg
    Bias Instability (1σ) 0.025 mg
    Angular Random Walk 0.025 m/s/ √h
    Scale Factor Non-Linearity 200 ppm
    Bias Run-Run (1σ) 0.1 mg

     

    Barometer
    Parameter value Unit
    Pressure range 450~1100 mbar
    50~1200 mbar
    Overall error 6 \
    Long-term stability 1 mbar/year

     

    Magnetometer
    Dynamic measurement range ±2 gauss
    Sensitivity 0.1 mgauss/LSB
    Initial sensitivity error 2 %
    Sensitivity temperature coefficient 250 ppm/℃
    Initial bias error 400 mgauss
    Partial temperature coefficient 0.7 mgauss/℃
    Output noise 4 mgauss
    Noise density 1 maguss/ √h
    Bandwidth 50-200 Hz

     

    GNSS
    Supported Navigation System BDS/GPS/GLONASS/Galileo/QZSS
    Main ANT Frequency BDS:B1L, B2L, B3L

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

    GLONASS: L1, L2

    Galileo: E1, E5a, E5b

    QZSS: L1, L2, L5

    Slave ANT Frequency BDS:B1L, B2L, B3L

    GPS:L1C/A, L2C

    GLONASS: L1, L2

    Galileo: E1, E5b

    QZSS: L1, L2

    Position Accuracy (RMS) Single point positioning Horizontal 1.5m
    Altitude 2.5m
    DGPS Horizontal 0.4m+1ppm
    Altitude 0.8m+1ppm
    RTK Horizontal 0.8cm+1ppm
    Altitude 1.5cm+1ppm
    Accuracy of observation (RMS)
    BDS GPS GLONASS Galileo
    B1I/L1 C/A/G1/E1 pseudo-range 10cm 10cm 10cm 10cm
    B1I/L1 C/A/G1/E1 Carrier Phase 1mm 1mm 1mm 1mm
    B3I/L2P(Y)/L2C/G2 pseudo-range 10cm 10cm 10cm 10cm
    B3I/L2P(Y)/L2C/G2 Carrier Phase 1mm 1mm 1mm 1mm
    B2I/L5/E5a/E5b pseudo-range 10cm 10cm 10cm 10cm
    B2I/L5/E5a/E5b Carrier Phase 1mm 1mm 1mm 1mm
    Time accuracy (RMS) 20ns
    Speed accuracy (RMS) 0.03m/s
    First positioning time <30s
    Initialization time <5s
    Data update rate <20Hz
    GNSS, MEMS INS, GNSS INS, MEMS
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