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CGM91AD10
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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.

Measurement Range

±450 °/s

In-Run Bias Stability

≤1.0 °/h

Angular Random Walk

≤0.12 °/√h

Product Gallery

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 undefined
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
Dimensions Drawingdimensions
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

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

CGM92AD10
MEMS / IMU

CGM92AD10

Measurement Range

±450 °/s

In-Run Bias Stability

≤1.5 °/h

Angular Random Walk

≤0.15 °/√h

Scale Factor Error

≤0.1 %

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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