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CGM300S10
Navigation / Mems / Imu

Tactical-Grade MEMS IMU with 0.05 °/h Gyro Bias Stability

MEMS Inertial Measurement Unit (IMU) · CGM300S10

Tactical-grade MEMS IMU integrating triaxial gyroscopes, accelerometers, and inclinometers with 0.05 °/h (1σ) gyro bias stability and 0.02 °/√h angular random walk. Factory-calibrated and temperature-compensated from −45 °C to +85 °C, with RS-422 output, external trigger, and 2000 g shock survivability for navigation and stabilization platforms.

Gyroscope Bias Stability (1σ)

0.05 °/hr

Angular Random Walk

0.02 °/√hr

Gyroscope Dynamic Range

±400 °/s

The CGM300S10 is a tactical-grade MEMS Inertial Measurement Unit (IMU) that combines high-performance gyroscopes, accelerometers, and inclinometers in a compact, rugged design. Featuring in-run gyro bias stability down to 0.05°/hr and angular random walk as low as 0.02°/√hr, it is built to meet the demands of high-precision navigation and control systems.

Its robust RS422 interface, small form factor, and wide operating temperature range make it an ideal solution for UAVs, robotics, surveying platforms, and autonomous vehicles, supporting both new designs and system upgrades.

Key Features

  • Tactical-grade IMU with **0.05°/hr** gyro bias stability
  • Integrated gyroscopes, accelerometers, and inclinometers
  • **9-axis fused output** with digital RS422 interface
  • Angular random walk down to **0.02°/√hr**
  • Fully calibrated and temperature-compensated output
  • Operates across **-45°C to +85°C**
  • Shock survivability up to **2000 g**
  • Compact and lightweight construction for easy integration

Applications

Unmanned Aerial Vehicles (UAVs)Robotics & Autonomous Ground Vehicles (UGVs)Surveying and Geospatial MappingPlatform and Gimbal StabilizationMarine & Subsea Navigation (AUVs)Industrial AutomationTactical Navigation SystemsLegacy system upgrades

Technical Specifications

Performance Specifications

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
Accelerometer Dynamic Range
±10 g
Inclinometer Dynamic Range
±1.7 g
Gyro Bandwidth (-3 dB)
150 Hz
Accelerometer Bandwidth (-3 dB)
100 Hz

Electrical and Environmental Specifications

Weight
120 g
Startup Time
1 s
Power Supply
4.5 – 5.5 V
Power Consumption
1.2 – 2.0 W
Startup Peak Current
700 mA
Communication Interface
RS422 —
Output Format
8-bit, No parity, 1 stop —
External Trigger
Supported —
Time of Validity (TOV) Signal
3.3V logic, active low —
Operating Temperature
-45 to +85 °C
Shock Tolerance
2000 g
  1. [1]Gyroscope and accelerometer bias stability figures are 1σ in-run values.
  2. [2]Bandwidth figures are −3 dB cutoff — 150 Hz gyroscope, 100 Hz accelerometer.

Package Information

Technical Drawings

D-Q-JDW-CGM300S10 Back View
Dimensions Drawingdimensions
D-Q-JDW-CGM300S10 Side View
Dimensions Drawingdimensions
D-Q-JDW-CGM300S10 Top View
Dimensions Drawingdimensions
D-Q-JDW-CGM300S10 Front View
Dimensions Drawingdimensions
D-Q-JDW-CGM300S10 Pins View
Pinout Diagrampinout

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Scale Factor Error

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CGM92AD10
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Scale Factor Error

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Full Temp Bias Variation

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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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