ChinaDrone.Request a quote ↗
COMPONENT

BW-IMU610

By Wuxi Beiwei Sensing Technology ↗

The Wuxi Beiwei Sensing Technology BW-IMU610 is a compact inertial measurement unit for navigation, attitude measurement and platform stabilization, including UAV integration. It combines gyroscope and accelerometer sensing with RS422 output, orthogonal compensation and temperature compensation. The standard accelerometer range is ±20g, with ±5g and ±50g options.

Request a quote ↗
Product identityBW-IMU610 series high-performance inertial measurement unit
DimensionsL44.8 × W38.6 × H21.5 mm
Orthogonal compensationOrthogonal compensation
Output interfaceRS422
Temperature range and compensation-40°C to +85°C; temperature compensation
Accelerometer measurement range±20gStandard accelerometer range.

Product overview

The Wuxi Beiwei Sensing Technology BW-IMU610 is an inertial sensing component for integration into navigation, attitude-measurement and stabilization systems. Its compact physical envelope measures 44.8 mm long, 38.6 mm wide and 21.5 mm high, defining the space occupied by the unit within a host assembly. The architecture includes gyroscope and accelerometer sensing, orthogonal compensation and an RS422 output interface. Intended applications span unmanned aircraft, underwater robot navigation, autonomous-driving navigation platforms, pipeline surveying, model attitude-angle measurement and platform stabilization.

The standard accelerometer range is ±20g, with ±5g and ±50g available as options; the gyroscope range is ±500°/s. The unit supports a maximum output frequency of 500Hz, with 200Hz bandwidth and a 200ms startup delay. Its temperature range is -40°C to +85°C, and temperature compensation is a stated feature. Performance conditions matter: the less than 1°/h gyroscope bias-stability figure uses 10s smoothing at room temperature, while the 10°/h full-temperature bias figure applies without temperature compensation.

Specifications

SpecificationValue & conditions
Product identityBW-IMU610 series high-performance inertial measurement unit
DimensionsL44.8 × W38.6 × H21.5 mm
Orthogonal compensationOrthogonal compensation
Output interfaceRS422
Temperature range and compensation-40°C to +85°C; temperature compensation
Accelerometer measurement range±20gStandard accelerometer range.
Accelerometer range options±5g or ±50gOptional accelerometer ranges.
Gyroscope resolution0.00006°/s
Gyroscope measurement range±500°/s
Gyroscope bias stabilityLess than 1°/hRoom temperature; 10s smoothing.
Gyroscope bias repeatabilityLess than 0.5°/hRoom temperature.
Gyroscope angular random walk0.05°/√hRoom temperature.
Gyroscope bias10°/hFull temperature range; without temperature compensation.
Gyroscope bandwidth200Hz
Maximum output frequency500Hz
Startup delay200ms
ApplicationsPipeline surveying; model attitude-angle measurement; platform stabilization; autonomous-driving navigation platforms; underwater robot navigation; unmanned aircraft
SOURCE WITH CHINADRONE

Request a quote for BW-IMU610

Send your application, destination country and expected quantity to the ChinaDrone team. We can discuss product selection, configuration and sourcing from China.

Submit your procurement requirements ↗

No account needed. A model number is optional. Your enquiry is handled by ChinaDrone.

KEEP EXPLORING

Similar products

Browse all products ↗
Flight control & navigation

BW-MINS327

By BWSENSING

The BWSENSING BW-MINS327 is a compact micro inertial navigation system for unmanned aircraft, robots, vehicles and stabilized platforms. Its 60 × 59 × 29 mm package provides gyroscope and accelerometer sensing, Kalman filtering and bias tracking, with a 9–36V DC supply and selectable interface outputs.

Flight control & navigation

BW-MINS527

By Wuxi Beiwei Sensing Technology

The Wuxi Beiwei Sensing Technology BW-MINS527 is a compact micro inertial navigation component for unmanned aircraft, vehicles and stabilization systems. It combines gyroscope and accelerometer sensing with selectable serial and Modbus outputs, 9–36V DC power, temperature compensation, and specified static and dynamic attitude accuracy.