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Tactical Grade MEMS Gyroscope Chip for Inertial Measurement Unit IMU INS

Tactical Grade MEMS Gyroscope Chip for Inertial Measurement Unit IMU INS

Brand Name:	Firepower
Model Number:	MGC150- P05
MOQ:	1
Price:	1500$
Payment Terms:	L/C,D/A,D/P,T/T,Western Union
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

China

Range:

150°/s

Bias Stability (10 S Smoothing):

0 .5°/h

Bias @ 25℃:

15°/h

Angle Random Walk:

0.06°/√ H

Bias Repeatability:

2°/h

Scale Factor Repeatability:

30ppmx

Non - Linearity @ Full Scale (FS):

100ppm

Bandwidth:

30Hz

Packaging Details:

BOX+Sponge

Supply Ability:

500/month

Product Description

Tactical Grade MEMS Gyroscope Chip for Inertial Measurement Unit IMU INS

0.5°/h bias stability for marine and stabilization applications

Key Specifications

Attribute	Value
Range	150°/s
Bias Stability (10 s smoothing)	0.5°/h
Bias @ 25℃	15°/h
Angle Random Walk	0.06°/√h
Bias Repeatability	2°/h
Scale Factor Repeatability	30ppmx
Non-linearity @ Full Scale (FS)	100ppm
Bandwidth	30Hz

Product Overview

The MGC series single-axis MEMS gyroscope chips are high-performance angular rate sensors designed for precision motion sensing applications. Housed in a compact and robust ceramic package, they feature a fully digital interface that simplifies integration into embedded systems.

With ultra-low bias instability down to 0.5°/h, angle random walk (ARW) as low as 0.06°/√h, and wide bandwidth, the MGC series offers exceptional performance in both dynamic and static environments. Their low noise density and high bias repeatability make them well-suited for applications requiring long-term stability, precision, and reliability.

Ideal Applications

Drones and unmanned aerial vehicles
Autonomous ground vehicles
Robotics and motion control platforms
Inertial Measurement Units
Inertial Navigation Systems
Missile and aerospace subsystems

Technical Parameters

Parameter	MGC150-P05	MGC500-P1	MGC500-P2	MGC500-P3	Unit
Range	150	500	500	500	dps
Bias @ 25℃	15	45	45	45	dph
Noise @ 10Hz	0.001	0.0012	0.0012	0.0012	mdps/√Hz
Bias Stability (10 s smoothing)	0.5	1.0	2.0	3.0	dph
Angle Random Walk	0.06	0.08	0.08	0.08	°/√h
Bias Repeatability (Weekly)	2	2	2	2	dph
Scale Factor	38550	11185	11185	11185	LSB/dps
Scale Factor Repeatability (Weekly)	30	30	30	30	ppm
Non-linearity @ Full Scale (FS)	100	100	100	100	ppm
Non-linearity @ 200 dps	50	50	50	50	ppm
Bandwidth	30	≥100	≥100	≥100	Hz
G-Sensitivity	2	3	3	3	dph/g
Vibration Rectification Coefficient @ 6.06 grms	0.4	0.3	0.3	0.3	dph/g²
Vibration Reliability (Power-on)	4000g, 0.5ms

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

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Tactical Grade MEMS Gyroscope Chip for Inertial Measurement Unit IMU INS

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