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MEMS Inertial Navigation System

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Product Detail

    MEMS inertial navigation system

    ER-MGI210 / 230 Closely integrated navigation system

    210-230.jpg

    ER-MGI210/230 Closely integrated navigation system can provide horizontal attitude, Heading attitude and other information, longitude, latitude, altitude, etc. positioning information, and the 3D acceleration, angular velocity inertial measurement information; and by extending the range of the mileage meter and the height of the barometer to further improve the accuracy and applicability of the system, can be widely used in unmanned aerial vehicles, vehicle navigation, aviation and platform stability control and other fields.


    ER-MGI230 use with high accuracy and high dynamic GPS receiver as the satellite signal sensor, using carrier phase differential technique and fast calculation of the whole week ambiguity technology, can accurately calculate the azimuth angle of the carrier motion; and inertial measurement technology aided attitude determination navigation, when the GPS signal is interference, by maintaining the inertial measurement unit, within a period of time, system can still output high precision data.


    ER-MGI230 overcomes the deficiency of a single device, give full play to the GPS high precision, no accumulation error, no drift, low price and inertial products good dynamic performance, strong anti-interference ability, without the need of external signal source are able to work and Improve the overall attitude measurement accuracy, navigation accuracy and real-time tracking performance of the system. The proof in the land, sea and air a variety of environmental test, heading accuracy of 0.1 degrees, roll and pitch accuracy 0.05 degrees, and effectively overcome the drift angle of heading error, it is multi system compatible and complement each other, mutual backup all-weather high reliability azimuth measurement products.Especially for In satellite communication vehicle, meteorological radar vehicle, warship, expedition ship, airship, UAV, fire control system, command and control system, weapon aiming system, have very strong competitiveness.


    Systematic   Name

    MGI210

    MGI230


    ER-MGI210

    ER-MGI230

    Performance Indicators

    Gyroscope

    Heading

    = 1.0 deg (1 s)

    = 0.3 deg (1 s)

    Range

    ±100 deg/s

    ±400 deg/s

    Horizontal   Attitude(Roll And Pitch)

    = 0.5 deg (1 s)

    = 0.2 deg (1 s)

    Bias Stability

    = 0.05 deg/s

    = 10 deg/h

    Horizontal   Position

    2.5   m CEP

    2.5   m CEP

    Bias   Repeatability

    = 0.05 deg/s

    = 10 deg/h

    Elevation

    4 m   CEP

    4 m   CEP

    Accelerometer

    Speed

    = 0.2 m/s (1 s)

    = 0.1 m/s (1 s)

    Range

    ±10 g(customizable)

    ±10g

    Interface Features

    Bias Stability

    = 0.1 mg

    = 0.1mg

    Voltage

    9~36   Vdc

    9~36   Vdc

    Bias   Repeatability

    = 0.2 mg

    = 0.2mg

    Power   Consumption

    = 3.5 W @ 12 VDC

    =4W @24Vdc

    GNSS

    Electrical   Interface

    RS232/RS422

    RS422

    Data   Update Rate

    100   Hz @ 115,200 bps

    100   ~ 200Hz

    GNSS   Features

    16   Channel, GPS

    L1   Frequency Point

    16   Channel GPSL1, 

    BD   B1

    Operating Environment

    Positioning   Time

    = 60 s

    = 60 s

    Operating Temperature

    -40° C ~ +85° C

    Typical   Recapture Time

    = 10 s

    = 10 s

    Storage Temperature

    -55° C ~ +85° C




    Vibration

    6 g   @ 20~2000 Hz




    Shock

    30   g, 11 ms, 1/2 Sine




    Physical Property




    Physical Size

    68.8×68×70 mm

    86.8×68×87 mm




    Weight

    = 500 g

    = 500 g






    ERICCO is expert in high quality mems ins manufacturing and selling, who is one of the best manufacturers and suppliers of mems ins with high precision. We have a professional factory at your service.

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Ericco International Limited

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