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6-DoF Tactical MEMS IMU with SPI Interface

MEMS Inertial Measurement Unit (IMU) · CGM91AD10

Tactical-grade 6-DoF MEMS IMU combining triaxial gyroscopes and accelerometers in a vacuum-sealed ceramic package. In-run bias stability ≤1.0 °/h (gyroscope) and ≤20 µg (accelerometer), with SPI digital interface, programmable FIR filtering, data rates up to 2460 SPS, and 10,000 g shock survivability.

Gyroscope SpecificationsMeasurement Range
±450 °/s
Accelerometer SpecificationsAccelerometer Measurement Range
±40 g
Gyroscope SpecificationsAngular Random Walk
≤0.12 °/√h
Read full specifications and measurement conditions ↓
6-DoF Tactical MEMS IMU with SPI Interface
CGM91AD10Product reference

Confirm configuration, interfaces and documentation with your inquiry.

The CGM91AD10 is a tactical-grade 6DoF inertial measurement unit (IMU), integrating triaxial gyroscopes and accelerometers in a sealed ceramic package. It delivers low-noise, stable data across −45°C to +85°C.

Factory calibration ensures excellent bias stability and minimal drift. With a digital SPI interface and integrated filtering, it offers easy system integration for advanced inertial applications.

Key Features

  • Fully calibrated triaxial gyroscope and accelerometer
  • Industry-leading in-run bias stability and random walk performance
  • Digital SPI interface with programmable FIR filtering and averaging
  • Robust ceramic vacuum package with enhanced noise isolation
  • High resistance to mechanical shock (up to 10,000 g survival)
  • Compact, lightweight form factor: optimized for embedded use
  • Configurable I/O, data-ready alarm, and external clock sync support
  • Single supply voltage operation (3.0 – 3.6 V)

Applications

Inertial Navigation Systems (INS)Unmanned Aerial Vehicles (UAVs)Platform Stabilization & ControlIndustrial RoboticsSurveying EquipmentGeophysical InstrumentationPersonnel and Asset Tracking

Technical Specifications

Gyroscope Specifications

Measurement Range
±450 °/s
In-Run Bias Stability
≤1.0 °/h
Angular Random Walk
≤0.12 °/√h
Scale Factor Error
≤0.05 %

Accelerometer Specifications

Accelerometer Measurement Range
±40 g
Accelerometer Bias Stability
≤20 μg
Velocity Random Walk
≤0.015 m/s/√h

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]Bias stability and random walk figures apply with factory calibration over the −45 °C to +85 °C operating range.
  2. [2]Maximum data rate (2460 SPS) depends on filter and decimation configuration.

Package Information

Technical Drawings

D-Q-JDW-CGM91AD10 Bottom View
Dimensions Drawingdimensions
D-Q-JDW-CGM91AD10 Top View
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D-Q-JDW-CGM91AD10 Front View
Dimensions Drawingdimensions
D-Q-JDW-CGM91AD10 Detail
Dimensions Drawingdimensions
D-Q-JDW-CGM91AD10 Pins View
Pinout Diagrampinout
D-Q-JDW-CGM91AD10 Pins Detail
Pinout Diagrampinout
D-Q-JDW-CGM91AD10 Pin Assignments
Pinout Diagrampinout

Frequently Asked Questions

What is CGM91AD10?+

Tactical-grade 6-DoF MEMS IMU combining triaxial gyroscopes and accelerometers in a vacuum-sealed ceramic package. In-run bias stability ≤1.0 °/h (gyroscope) and ≤20 µg (accelerometer), with SPI digital interface, programmable FIR filtering, data rates up to 2460 SPS, and 10,000 g shock survivability.

Which specifications are published for CGM91AD10?+

Gyroscope Specifications — Measurement Range: ±450 °/s; Gyroscope Specifications — In-Run Bias Stability: ≤1.0 °/h; Gyroscope Specifications — Angular Random Walk: ≤0.12 °/√h. Measurement conditions: Bias stability and random walk figures apply with factory calibration over the −45 °C to +85 °C operating range. Maximum data rate (2460 SPS) depends on filter and decimation configuration. 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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