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Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System

Shenzhen Fire Power Control Technology Co., LTD
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    Buy cheap Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System from wholesalers
     
    Buy cheap Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System from wholesalers
    • Buy cheap Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System from wholesalers
    • Buy cheap Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System from wholesalers
    • Buy cheap Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System from wholesalers
    • Buy cheap Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System from wholesalers
    • Buy cheap Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System from wholesalers
    • Buy cheap Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System from wholesalers

    Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System

    Ask Lasest Price
    Brand Name : Firepower
    Model Number : MG3-1A
    Certification : CE
    Price : Negotiable
    Payment Terms : T/T
    Supply Ability : 500/month
    Delivery Time : 10 days
    • Product Details
    • Company Profile

    Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System

    MG3-1A MEMS Gyroscope is a fully integrated 3-axis angular rate sensor designed for precision inertial navigation, UAV guidance, and robotic motion control.
    It consists of a 3-axis MEMS gyroscope, temperature sensor, signal processing board, structural components, and dedicated software, delivering temperature-compensated, alignment-corrected, and linearity-corrected angular rate data through RS-422.
    With a measuring range of ±400°/s, zero-bias instability of 0.3°/h, random walk of 0.15°/√h, and start-up time of 17 s, the MG3-1A is perfect for UAVs, autonomous survey platforms, mobile robotics, and precision navigation instruments.
    As a Stim210 compatible replacement, it provides a compact (52 g), reliable, and high-precision solution for civilian and research INS applications.


    Main technical parameters

    1.2.1 Technical index of gyroscope

    Parameter

    Unit

    Test conditions

    MG3-1A

    MG3-1C

    MG3-1E

    Measuring range

    °/s

    ±400

    ±400

    ±300

    Zero-bias instability

    °/h

    Allan variance

    0.3

    0.1

    0.2

    Zero bias stability

    °/h

    10s smooth, RMS, Room temperature

    3

    1

    1

    Zero bias variation at full temperature

    °/h

    10s smoothing, RMS, temperature change rate

    1℃/min

    20

    10

    5

    Random walk

    °/√h

    Allan variance

    0.15

    0.05

    0.03

    Output noise

    p-p

    Peak (Half Peak, RMS * 3)

    0.3

    0.25

    0.2

    Zero-bias repeatability

    °/h

    Q = 6, Room temperature

    3

    1

    0.5

    Zero bias acceleration sensitivity

    Test at ± 1 g

    2

    2

    2

    Resolution

    °/h

    2

    1

    1

    Bandwidth

    Hz

    250

    250

    400

    Scale factor nonlinearity

    ppm

    Room temperature

    100

    Scale factor repeatability

    ppm

    Q = 3, Room temperature

    100

    Cross coupling

    %

    Room temperature

    0.1

    1.2.2 Electrical characteristics

    Parameter

    Unit

    MG3-1A

    Voltage

    V

    +5±0.25

    Startup current

    mA

    400

    Steady-state power consumption

    W

    1.4

    Ripple

    mV

    100

    1.2.3 Environmental adaptability

    Parameter

    Unit

    MG3-1A

    Operating temperature

    -45~85

    Storage temperature

    -55~105

    1.2.4 Others

    Parameter

    Unit

    MG3-1A

    Weight

    g

    52±5

    Start time

    s

    1

    Overall dimension



    Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System

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