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BW-MINS525

By BWSENSING ↗

The BWSENSING BW-MINS525 is a packaged CAN-bus micro inertial navigation unit for unmanned aircraft, robotics and platform stabilization. Its 60 × 59 × 29 mm housing integrates gyroscope and accelerometer functions, with 9–36V DC power, temperature compensation and separate dynamic, static and heading-retention specifications.

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Product typeBW-MINS525 ultra-high-precision CAN-bus micro inertial navigation system
Dynamic attitude accuracy0.1°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.1°/min
Gyroscope resolution0.01°/sec

Product overview

The BWSENSING BW-MINS525 is a compact CAN-bus micro inertial navigation system intended for integration into unmanned aircraft, robotic equipment and other mobile platforms. Its packaged housing measures 60 mm long, 59 mm wide and 29 mm high, defining the physical space needed for the sensor unit. The hardware combines gyroscope and three-axis accelerometer functions with attitude measurement. Integration provisions include CAN output and a 9–36V DC supply input, while temperature compensation accompanies a specified range of -40℃ to +85℃.

Attitude specifications distinguish 0.1° dynamic accuracy from 0.01° static accuracy, with pitch coverage of ±90º and roll coverage of ±180º. Heading retention is specified at 0.1°/min. Processing includes Kalman filtering and a dedicated bias-tracking algorithm for drift elimination. Gyroscope bias stability is 5°/h across the full temperature range under a 10s, 1σ condition. Accelerometer bias stability has separate 25℃ values for 100s and 10s intervals, so those figures retain their respective measurement conditions when assessing integration requirements.

Specifications

SpecificationValue & conditions
Product typeBW-MINS525 ultra-high-precision CAN-bus micro inertial navigation system
Dynamic attitude accuracy0.1°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.1°/min
Gyroscope resolution0.01°/sec
Gyroscope bias stability5°/hFull temperature range; 10s, 1σ.
Angular random walk coefficientLess than 0.1 °/√h
Accelerometer 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 DCDC supply.
Output interfaceCAN
Temperature range-40℃ to +85℃Temperature compensation.
DimensionsL60 × W59 × H29 mmPackaged product.
Bias trackingSpecial bias-tracking algorithm for drift elimination
FilteringHigh-performance Kalman filtering algorithm
ApplicationsUnmanned boats and underwater vehicles; robotics; platform stabilization; large vessels; automated guided vehicles; automated and unmanned driving; special-purpose vehicles; unmanned aircraft
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