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CGM92AD10
Navigation / Mems / Imu

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.

Measurement Range

±450 °/s

In-Run Bias Stability

≤1.5 °/h

Angular Random Walk

≤0.15 °/√h

Product Gallery

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 undefined

Barometer Specifications

Pressure Range
300–1100 mbar
Resolution
0.012 mbar

General Specifications

Data Rate
Up to 2460 SPS
Digital Interface
SPI undefined
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
Dimensions Drawingdimensions
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

Related Products

CGM300S10
MEMS / IMU

CGM300S10

Gyroscope Bias Stability (1σ)

0.05 °/hr

Angular Random Walk

0.02 °/√hr

Gyroscope Dynamic Range

±400 °/s

Accelerometer Bias Stability (1σ)

0.01 mg

CGM91AD10
MEMS / IMU

CGM91AD10

Measurement Range

±450 °/s

In-Run Bias Stability

≤1.0 °/h

Angular Random Walk

≤0.12 °/√h

Scale Factor Error

≤0.05 %

CGM66EK10
MEMS / IMU

CGM66EK10

Measurement Range

— °/s

Bias Instability

Allan Variance °/h

Bias Stability

1s smoothing, RMS, room temperature °/h

Full Temp Bias Variation

10s smoothing, RMS, temp rate 1°C/min °/h

Technical Documentation

Detailed documentation is shared directly with qualified B2B buyers after inquiry, under mutual confidentiality. Customer, supplier, and program information is never published.

Include the model number and your application in the inquiry form — an engineer will respond with the relevant documents.

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Datasheet (PDF)

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

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