ChinaDrone.Request a quote ↗
COMPONENT

BW-MINS225

By Wuxi Beiwei Sensing Technology ↗

The Beiwei Sensing BW-MINS225 is a compact CAN bus micro inertial navigation system for unmanned aircraft, robots and mobile platforms. Its packaged gyroscope and accelerometer hardware occupies 60 × 59 × 29 mm, accepts 9–36V DC power and provides attitude measurement with temperature compensation, Kalman filtering and bias tracking.

Request a quote ↗
Manufacturer and modelBeiwei Sensing BW-MINS225 micro inertial navigation system
Dynamic attitude accuracy0.5°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.3°/60s
Gyroscope resolution0.01°/sec

Product overview

The Beiwei Sensing BW-MINS225 is a packaged micro inertial navigation system for integration into unmanned aircraft, robotic equipment and other moving platforms. Its sensing architecture includes gyroscope and accelerometer functions, with CAN bus output for connection to host equipment. The enclosure measures 60 mm long, 59 mm wide and 29 mm high, providing a defined physical envelope for installation planning. Electrical integration requires a 9–36V DC supply, while the temperature-compensated operating range extends from -40℃ to +85℃.

Attitude measurement covers pitch through ±90º and roll through ±180º, with dynamic accuracy of 0.5° and static accuracy of 0.01°. Heading retention is specified as 0.3°/60s. Processing combines Kalman filtering with a bias-tracking algorithm for drift removal. The accelerometer range is ±1.8 g on each of three axes. Its bias-stability figures depend on the stated temperature and observation interval, while the gyroscope’s full-temperature bias stability is specified at 10 seconds and one standard deviation. These conditions distinguish the individual performance figures.

Specifications

SpecificationValue & conditions
Manufacturer and modelBeiwei Sensing BW-MINS225 micro inertial navigation system
Dynamic attitude accuracy0.5°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.3°/60s
Gyroscope resolution0.01°/sec
Gyroscope bias stability20°/hFull temperature range; 10s, 1σ.
Angular random walk coefficientLess than 0.1 °/√h
Accelerometer measurement range±1.8 gX, Y and Z axes.
Accelerometer bias stability over 100 seconds0.001mg25℃, 100s, 1σ.
Accelerometer bias stability over 10 seconds0.01mg25℃, 10s, 1σ.
Supply voltage9–36V DC
Output interfaceCAN bus
Temperature range-40℃ to +85℃Temperature compensated.
DimensionsL60 × W59 × H29 mmPackaged product.
Bias trackingSpecial bias-tracking algorithm for drift removal
FilteringHigh-performance Kalman filtering algorithm
ApplicationsUnmanned boats and underwater vehicles; robots; platform stabilization; large ships; automated guided vehicles; automated and driverless driving; special-purpose vehicles; unmanned aircraft
SOURCE WITH CHINADRONE

Request a quote for BW-MINS225

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-IMU225E

By BWSENSING

The BWSENSING BW-IMU225E is a CAN inertial measurement unit for unmanned aircraft, robotics and vehicle integration. Packaged and bare-board configurations provide different installation envelopes. It combines gyroscope and accelerometer measurements with 500 Hz output, a 9–36 V DC supply range, temperature compensation and specified electrical immunity ratings.

GEPRC TAKER F722 BLS 80A 8S STACK flight controller and ESC assembly
Flight control & navigation

GEPRC TAKER F722 BLS 80A 8S STACK

By GEPRC

The GEPRC TAKER F722 BLS 80A 8S STACK is a UAV electronics assembly pairing an F722 flight controller with an 80A four-in-one ESC. It accepts 3-8S LiPo power and provides dual regulated supplies, six UARTs and direct DJI Air Unit connectivity. The stack configuration includes filtering, wiring and mounting hardware.

Bynav Gmouse module-integrated RTK antenna shown from below with mounting hardware.
Flight control & navigation

Bynav Gmouse Module-integrated RTK Antenna

By Bynav

The bynav Gmouse Module-integrated RTK Antenna is an integrated GNSS/INS positioning component for machinery and unmanned-system integration. Its Gmouse-M20, M21 and M22 configurations combine an M2-series module with antenna hardware; built-in positioning electronics and inertial sensing support high-precision navigation, with configuration-dependent output rates and qualified accuracy specifications.