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CGM66EK10
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MEMS IMU with RS-422 Output and Full-Temperature Compensation

MEMS Inertial Measurement Unit (IMU) · CGM66EK10

Compact MEMS inertial measurement unit integrating a three-axis gyroscope, three-axis accelerometer, temperature sensor, and embedded compensation algorithms with RS-422 digital output. Full-temperature bias compensation from −45 °C to +85 °C, 1-second startup, and low power consumption for stabilization and navigation integration.

Measurement Range

— °/s

Bias Instability

Allan Variance °/h

Bias Stability

1s smoothing, RMS, room temperature °/h

The CGM66EK10 is a compact, lightweight MEMS Inertial Measurement Unit (IMU) that integrates a three-axis gyroscope, three-axis accelerometer, temperature sensor, and embedded compensation algorithms. It delivers precise angular rate, acceleration, and tilt measurements via an RS-422 digital interface, making it ideal for applications requiring high dynamic performance and stability.

With its advanced temperature compensation and low power consumption, this device provides reliable performance in space-constrained applications while maintaining high accuracy across a wide temperature range.

Key Features

  • Tri-axis gyroscope and accelerometer
  • Full temperature range bias compensation
  • High bias stability and low random walk
  • RS-422 digital communication
  • External TTL trigger support
  • Fast 1-second startup
  • Low power consumption
  • Compact and rugged design

Applications

Unmanned aerial vehicles (UAVs) and roboticsPrecision agriculturePlatform stabilization and gimbal controlIndustrial automation and equipment monitoringInertial navigation and motion tracking

Technical Specifications

Gyroscope Specifications

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
Angle Random Walk
Allan Variance °/√h
Bias Repeatability
Q = 6, room temperature °/h
Acceleration Sensitivity
Under ±1g °/h/g
Resolution
— °/h
Output Noise
Peak (3σ) °/s
Scale Factor Nonlinearity
Room temperature ppm
Scale Factor Repeatability
Q = 3, room temperature ppm
Cross-Axis Sensitivity
Room temperature %
Bandwidth
— Hz

Accelerometer Specifications

Accelerometer Measurement Range
— g
Accelerometer Bias Stability
1s smoothing, RMS, room temperature mg
Full Temp Bias Variation
10s smoothing, RMS, temp rate 1°C/min mg
Bias Repeatability
Q = 6, room temperature mg
Resolution
— mg
Scale Factor Nonlinearity
Room temperature ppm
Scale Factor Repeatability
Q = 3, room temperature ppm
Cross-Axis Sensitivity
Room temperature %
Bandwidth
— Hz

Electrical and Environmental Specifications

Weight
120 g
Startup Time
1 s
Input Voltage
+5 ± 0.5 V
Startup Current
< 400 mA
Power Consumption
< 1.2 W
Power Ripple
100 mV
Operating Temperature
-45 to +85 °C
Storage Temperature
-55 to +105 °C
  1. [1]Bias instability and angular random walk are characterized by Allan variance; bias stability figures are 1 s smoothing RMS at room temperature.
  2. [2]Full-temperature bias variation is specified at a temperature rate of 1 °C/min with 10 s smoothing RMS.
  3. [3]Per-axis and per-range values are confirmed for the delivered configuration.

Package Information

Technical Drawings

D-Q-JDW-CGM66EK10 Side View
Dimensions Drawingdimensions
D-Q-JDW-CGM66EK10 Top View
Dimensions Drawingdimensions
D-Q-JDW-CGM66EK10 Bottom View
Dimensions Drawingdimensions
D-Q-JDW-CGM66EK10 Pins View
Pinout Diagrampinout

Related Products

CGM300S10
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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
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CGM91AD10

Measurement Range

±450 °/s

In-Run Bias Stability

≤1.0 °/h

Angular Random Walk

≤0.12 °/√h

Scale Factor Error

≤0.05 %

CGM92AD10
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CGM92AD10

Measurement Range

±450 °/s

In-Run Bias Stability

≤1.5 °/h

Angular Random Walk

≤0.15 °/√h

Scale Factor Error

≤0.1 %

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.

picture_as_pdf

Datasheet (PDF)

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

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