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Accelerometer Gyro Sensor
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Industrial-grade single-axis MEMS gyroscope chips for Unmanned Systems

Industrial-grade single-axis MEMS gyroscope chips for Unmanned Systems

Brand Name: Firepower
Model Number: MGC500- P1
MOQ: 1
Price: 1500$
Payment Terms: L/C,D/A,D/P,T/T,Western Union
Supply Ability: 500/month
Detail Information
Place of Origin:
China
Range:
500°/s
Bias Stability (10 S Smoothing):
1°/h
Bias @ 25℃:
45°/h
Angle Random Walk:
0.08°/√ H
Bias Repeatability:
2°/h
Scale Factor Repeatability:
30ppmx
Non - Linearity @ Full Scale (FS):
100ppm
Bandwidth:
100Hz
Packaging Details:
BOX+Sponge
Supply Ability:
500/month
Highlight:

Unmanned Systems gyroscope chips

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single-axis MEMS gyroscope chips

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Tactical-grade gyroscope chips

Product Description
Tactical-grade Single-axis MEMS Gyroscope Chips for Unmanned Systems
Product Overview

The MGC series single-axis MEMS gyroscopes deliver highly stable and low-noise angular velocity outputs in a compact ceramic package with fully digital interface. With bias stability as low as 1 dph, angle random walk down to 0.08°/√h, and wide bandwidth up to ≥100 Hz, these sensors are ideal for demanding applications requiring high precision and long-term repeatability.

Technical Parameters
Parameter MGC500-P1 MGC500-P2 MGC500-P3 Unit
Range 500 500 500 dps
Bias @ 25℃ 45 45 45 dph
Noise @ 10Hz 0.0012 0.0012 0.0012 mdps/√Hz
Bias Stability (10 s smoothing) 1.0 2.0 3.0 dph
Angle Random Walk 0.08 0.08 0.08 °/√h
Bias Repeatability (Weekly) 2 2 2 dph
Scale Factor 11185 11185 11185 LSB/dps
Scale Factor Repeatability (Weekly) 30 30 30 ppm
Non-linearity @ Full Scale (FS) 100 100 100 ppm
Non-linearity @ 200 dps 50 50 50 ppm
Bandwidth ≥100 ≥100 ≥100 Hz
G-Sensitivity 3 3 3 dph/g
Typical Applications
  • Inertial Navigation Systems
  • Platform Stabilization
  • Attitude and Heading Reference System
  • Precision Agriculture and Industrial Automation
  • UAV and Autonomous Vehicle Systems

Ideal for drone and unmanned systems' orientation and attitude control, as well as for integration into advanced navigation systems such as IMU and INS.