HG3900 MEMS Inertial Measurement Unit
The HG3900 is designed and built at a Honeywell Aerospace facility in the USA. It typically has an ECCN of 7A003.d.1 but can vary depending on model selected. It generally requires an export license
Specifications
Key Benefits
- All silicon MEMS IMU with superior performance vs. similar size RLG and FOG based IMUs
- Highly robust, ruggedized to tolerate high vibration, shock and dynamic thermal environments
- Performance has been validated over full environments by U.S. Army/NTA labs
- Reduced Size & Power
- SMALLER, LOWER POWER, HIGHER PERFORMANCE IMUs than available in FOG, RLG & Quartz-MEMS based IMUs today; with RELIABLE Performance throughout the product life without repair or overhaul.
- Small size (3.1 x 3.0 inches), and low weight (less than 2 pounds)
- The HG3900 offers many factory configurable features, such as data rate output, output message protocol, and flight control filtering, to simplify system integration.
Accel Bias In-Run Stability (mg 1σ)
- 0.050
Gyro sensor technology
- MEMS
Gyro Operating Range
- 1074°/sec
Gyro Bias Repeatability
- 0.5 °∕hr 1σ
Gyro Bias In-Run Stability
- 0.08 °∕hr 1σ
Gyro ARW
- 0.015
Accelerometer Sensor Technology
- MEMS
Accelerometer Operating Range
- 37
Accel Bias Repeatability (mg 1σ)
- 0.5
Accel Velocity Random Walk (VRW)
- .02
Weight
- <907 g
Dimensions
- 75mm diameter x 79mm H (not inclusive of mounting tabs)
Supply Voltage
- 5VDC and +15VDC
Power Consumption
- <6 W Watt
Operating Temperature
- -40C to +71°C (Inertial Performance), -54C to +85C (Control Performance)
Data Rate
- 600Hz Control/100Hz Inertial
Communication Protocols
- SDLC, ASYNC
Communication Ports
- RS-422 compatible TXD output