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Asset ID: quartz-mems-imu-cgsm40cj1
CGSM40CJ11
Navigation / Quartz Mems / Imu

CGSM40CJ11

Three-axis quartz MEMS gyroscope and accelerometer integrated IMU, high reliability, compact, for navigation and industrial applications.

Power Supply Voltage

V 5 ± 0.2

Operating Current

mA 19 ± 5

Weight

g 12 ± 5

Product Gallery

The CGSM40CJ1A is a compact, high-reliability inertial measurement unit integrating three orthogonally mounted quartz MEMS gyroscopes, three-axis MEMS accelerometers, and digital control circuitry. Advanced compensation for bias, scale factor, and installation errors enables precise angular velocity and acceleration measurement in aerospace, navigation, industrial, and marine applications.

Key Features

  • Integrated three-axis quartz MEMS gyroscope and accelerometer
  • Advanced digital compensation and calibration
  • Compact and lightweight
  • Wide operating temperature range
  • High bias stability and repeatability
  • Suitable for aerospace, navigation, and industrial control

Applications

Inertial navigationMotion and attitude measurementAerospace and marine equipmentIndustrial control systems

Technical Specifications

General Specifications

Power Supply Voltage

V

5 ± 0.2

Operating Current

mA

19 ± 5

Weight

g

12 ± 5

Startup Time

s

≤2

Gyroscope Specifications

Measurement Range

°/s

±300

Scale Factor

-

1 ± 0.005

Scale Factor Nonlinearity

ppm

≤200

Scale Factor Repeatability

ppm

≤200

Scale Factor Asymmetry

ppm

≤200

Cross-Axis Sensitivity

-

≤0.005

Threshold / Resolution

°/s

≤0.005

Bias (Full Temperature)

°/s

±0.05

Bias Stability (Room Temp)

°/h

≤10

Bias Stability (Full Temp)

°/h

≤50

Bias Repeatability

°/h

≤15

Angular Random Walk

°/√h

≤0.08

Bias Instability (Allan Deviation)

°/h

≤2

Bandwidth (Amplitude)

Hz

200

Delay Time

ms

√2.0

Accelerometer Specifications

Measurement Range

g

±110

Bias (Full Temperature)

mg

±10

Bias Stability (Room Temp)

mg

≤0.1

Bias Stability (Full Temp)

mg

≤1

Bias Repeatability

mg

≤0.1

Environmental Adaptability

Vibration (Gyroscope, 6.06g RMS)

°/h

≤36

Shock (Gyroscope, 200g, 6ms)

°/h

≤36

Vibration (Accelerometer)

mg

≤10

Shock (Accelerometer)

mg

≤10

Operating Temperature

-45 ~ +85

Storage Temperature

-55 ~ +85

General Specifications

Power Supply Voltage

V

5 ± 0.2

Operating Current

mA

18 ± 4

Weight

g

≤20

Startup Time

s

≤2

Gyroscope Specifications

Measurement Range

°/s

±300

Scale Factor

-

1 ± 0.005

Scale Factor Nonlinearity

ppm

≤200

Scale Factor Repeatability

ppm

≤200

Scale Factor Asymmetry

ppm

≤200

Cross-Axis Sensitivity

-

≤0.005

Threshold / Resolution

°/s

≤0.005

Bias (Full Temperature)

°/s

±0.05

Bias Stability (Room Temp)

°/h

≤10

Bias Stability (Full Temp)

°/h

≤30

Bias Repeatability

°/h

≤10

Angular Random Walk

°/√h

≤0.2

Bias Instability (Allan Deviation)

°/h

≤2

Bandwidth (Amplitude)

Hz

120

Delay Time

ms

√2.0

Accelerometer Specifications

Measurement Range

g

±16

Bias (Full Temperature)

mg

±5

Bias Stability (Room Temp)

mg

≤0.2

Bias Stability (Full Temp)

mg

≤1

Bias Repeatability

mg

≤0.4

Environmental Adaptability

Vibration (Gyroscope, 6.06g RMS)

°/h

≤36

Shock (Gyroscope, 200g, 6ms)

°/h

≤36

Vibration (Accelerometer)

mg

Shock (Accelerometer)

mg

≤10

Operating Temperature

-40 ~ +80

Storage Temperature

-45 ~ +85

Package Information

Technical Drawings

Quartz MEMS IMU CGSM40CJ1A
Dimensions Drawingdimensions
Quartz MEMS IMU CGSM40CJ11
Dimensions Drawingdimensions

Technical Documentation

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Datasheet (PDF)

Full performance curves, pinout diagrams, and environmental testing results.

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CAD Model (STEP)

High-fidelity 3D geometry for structural integration and thermal modeling.

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Compliance Documentation

Certification of origin, quality management protocols, and compliance documentation.

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All specifications can be customized. Tell us your requirements for a tailored solution.