MEMS 3 Axis Inertial Sensor for Vehicle and Aerospace Navigation

Brand Name:Firepower
Certification:CE
Model Number:MG3-1A
Minimum Order Quantity:1
Delivery Time:10 days
Payment Terms:T/T
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Location: Shenzhen Guangdong China
Address: 429, Building A10, Fuhai Information Port, Xinhe Community, Fuhai Street, Shenzhen, Guangdong, China
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Product Details

MG3-1A MEMS Gyroscope is a fully integrated 3-axis angular rate sensor offering high precision and reliability for UAVs, autonomous navigation systems, and robotic platforms.
It combines a 3-axis MEMS gyroscope, temperature sensor, signal processing board, and structural framework with advanced software for error compensation. Angular rate data is output via RS-422, supporting temperature compensation, alignment correction, and nonlinear calibration.
Technical highlights include a ±400°/s measuring range, zero-bias stability of 3°/h, bandwidth up to 250 Hz, and low random walk (0.15°/√h), making it perfect for precision motion control, UAV navigation, drone attitude stabilization, and survey instruments.
This gyroscope is a Stim210 replacement, delivering a compact, lightweight (52 g), high-performance 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



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MEMS 3 Axis Inertial Sensor for Vehicle and Aerospace Navigation

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