China Navigation Grade MEMS Stim 210  Angular Rate Sensor for Navigation System for sale
China Navigation Grade MEMS Stim 210  Angular Rate Sensor for Navigation System for sale
China Navigation Grade MEMS Stim 210  Angular Rate Sensor for Navigation System for sale
China Navigation Grade MEMS Stim 210  Angular Rate Sensor for Navigation System for sale
China Navigation Grade MEMS Stim 210  Angular Rate Sensor for Navigation System for sale
China Navigation Grade MEMS Stim 210  Angular Rate Sensor for Navigation System for sale
China Navigation Grade MEMS Stim 210  Angular Rate Sensor for Navigation System for sale

Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System

Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System The MG3-1A MEMS Gyroscope is a fully integrated 3-axis angular rate sensor designed for precision inertial navigation, UAV guidance, and robotic motion control . This system 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

Place of Origin China
Angle Random Walk 0.15°/√h
Packaging Details sponge and carton
Range 400deg/s
Model Number MG3-1A
Bias Stability 0.3°/h
Product Description
Navigation Grade MEMS Stim 210 Angular Rate Sensor for Navigation System

The MG3-1A MEMS Gyroscope is a fully integrated 3-axis angular rate sensor designed for precision inertial navigation, UAV guidance, and robotic motion control.

This system 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 ideal 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 Other Specifications
Parameter Unit MG3-1A
Weight g 52±5
Start time s 1
Overall Dimensions
MG3-1A MEMS Gyroscope dimensions and physical appearance
Interested in this product?
Contact us now for more details and a custom quote.