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10-DoF MEMS IMU with Magnetometer and Barometer

MEMS Inertial Measurement Unit (IMU) · CGM92AD10

Tactical-grade 10-DoF MEMS IMU integrating triaxial gyroscopes, accelerometers, magnetometers, and a barometric pressure sensor in a vacuum-sealed ceramic package. SPI interface with data rates up to 2460 SPS, factory calibration, −45 °C to +85 °C operation, and 10,000 g shock survivability for navigation, stabilization, and survey instrumentation.

Gyroscope SpecificationsMeasurement Range
±450 °/s
Magnetometer SpecificationsMeasurement Range
±8 Gauss
Accelerometer SpecificationsAccelerometer Measurement Range
±40 g
Read full specifications and measurement conditions ↓
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10-DoF MEMS IMU with Magnetometer and Barometer
CGM92AD10Product reference

Confirm configuration, interfaces and documentation with your inquiry.

The CGM92AD10 is a tactical-grade 10DoF inertial measurement unit integrating gyroscopes, accelerometers, magnetometers, and a barometric pressure sensor in a compact, vacuum-sealed ceramic package. It provides low-noise, stable inertial and environmental measurements across −45°C to +85°C.

Factory-calibrated and ready for integration, **CGM92AD10** is ideal for navigation, stabilization, and sensing in challenging environments.

Key Features

  • Full 10DoF sensing: gyroscope, accelerometer, magnetometer, barometer
  • Factory-calibrated for bias, sensitivity, and alignment
  • Low in-run bias drift and angular random walk
  • SPI digital interface, up to 2.46 kSPS
  • Built-in FIR filtering and data decimation
  • Operating temperature: −45°C to +85°C
  • Shock survivability up to 10,000 g
  • Single 3.0–3.6 V power supply

Applications

Inertial navigation and GNSS aidingUAV and robotics guidancePlatform and gimbal stabilizationOil & gas downhole toolsMining and geophysical surveyingMobile mapping and autonomous vehicles

Technical Specifications

Gyroscope Specifications

Measurement Range
±450 °/s
In-Run Bias Stability
≤1.5 °/h
Angular Random Walk
≤0.15 °/√h
Scale Factor Error
≤0.1 %

Accelerometer Specifications

Accelerometer Measurement Range
±40 g
Accelerometer Bias Stability
≤25 μg
Velocity Random Walk
≤0.02 m/s/√h

Magnetometer Specifications

Measurement Range
±8 Gauss
Resolution
High

Barometer Specifications

Pressure Range
300–1100 mbar
Resolution
0.012 mbar

General Specifications

Data Rate
Up to 2460 SPS
Digital Interface
SPI
Power Supply
3.0–3.6 V
Operating Temperature
-45~+85 °C
Shock Survivability
10000 g
  1. [1]Gyroscope in-run bias stability (≤1.5 °/h) and angular random walk (≤0.15 °/√h) are factory-calibrated figures over the operating temperature range.

Package Information

Technical Drawings

D-Q-JDW-CGM92AD10 Overview
Dimensions Drawingdimensions
D-Q-JDW-CGM92AD10 Bottom View
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D-Q-JDW-CGM92AD10 Detail A
Dimensions Drawingdimensions
D-Q-JDW-CGM92AD10 Front View
Dimensions Drawingdimensions
D-Q-JDW-CGM92AD10 Detail B
Dimensions Drawingdimensions
D-Q-JDW-CGM92AD10 Pins View
Pinout Diagrampinout
D-Q-JDW-CGM92AD10 Pins Detail
Pinout Diagrampinout
D-Q-JDW-CGM92AD10 Pin Assignments
Pinout Diagrampinout

Frequently Asked Questions

What is CGM92AD10?+

Tactical-grade 10-DoF MEMS IMU integrating triaxial gyroscopes, accelerometers, magnetometers, and a barometric pressure sensor in a vacuum-sealed ceramic package. SPI interface with data rates up to 2460 SPS, factory calibration, −45 °C to +85 °C operation, and 10,000 g shock survivability for navigation, stabilization, and survey instrumentation.

Which specifications are published for CGM92AD10?+

Gyroscope Specifications — Measurement Range: ±450 °/s; Gyroscope Specifications — In-Run Bias Stability: ≤1.5 °/h; Gyroscope Specifications — Angular Random Walk: ≤0.15 °/√h. Measurement conditions: Gyroscope in-run bias stability (≤1.5 °/h) and angular random walk (≤0.15 °/√h) are factory-calibrated figures over the operating temperature range. See the technical specifications for the complete parameter list.

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Supporting information

Documentation,
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Detailed documentation is shared directly with qualified B2B buyers after inquiry, under mutual confidentiality. Include the model and your application.

  • Datasheet (PDF)

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

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