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BW-MINS225

By BWSENSING ↗

The BWSENSING BW-MINS225 is a compact CAN bus miniature inertial navigation system for integration into unmanned aircraft and other mobile or stabilized equipment. Its 60 × 59 × 29 mm package provides gyroscope and accelerometer functions, temperature compensation, bias tracking and Kalman filtering, with 9–36V DC power and a -40℃ to +85℃ temperature range.

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Product identity and typeBWSENSING BW-MINS225 CAN bus miniature inertial navigation system
Dynamic attitude accuracy0.5°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading holding accuracy0.3°/60s
Gyroscope resolution0.01°/sec

Product overview

The BWSENSING BW-MINS225 is a miniature inertial navigation system intended for integration into unmanned aircraft, robots, marine vehicles and stabilization platforms. Its packaged architecture combines gyroscope and accelerometer measurement functions with CAN output, bias tracking and Kalman filtering. The enclosure measures 60 × 59 × 29 mm, defining the component’s physical integration space. Electrical integration uses a 9–36V DC supply and a CAN interface, while temperature compensation accompanies a specified temperature range of -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 holding accuracy is 0.3°/60s. The accelerometer range is ±1.8 g on each of the X, Y and Z axes. Its bias stability figures carry distinct measurement conditions: 0.001mg at 25℃ over 100s and 0.01mg at 25℃ over 10s, both at 1σ. Gyroscope bias stability across the full temperature range is 20°/h at 10s and 1σ.

Specifications

SpecificationValue & conditions
Product identity and typeBWSENSING BW-MINS225 CAN bus miniature inertial navigation system
Dynamic attitude accuracy0.5°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading holding 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 at 100s0.001mg25℃, 100s, 1σ.
Accelerometer bias stability at 10s0.01mg25℃, 10s, 1σ.
Supply voltage9–36V DC
Output interfaceCAN
Temperature range-40℃ to +85℃Temperature compensated.
Drift compensationSpecial bias tracking algorithm for drift elimination
FilteringHigh performance Kalman filtering algorithm
Dimensions60 × 59 × 29 mmPackaged product; length × width × height.
ApplicationsUnmanned surface vessels and underwater vehicles; robots; platform stabilization; large ships; automated guided vehicles; automated and driverless operation; special vehicles; unmanned aircraft
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