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BW-MINS325

By BWSENSING ↗

The BWSENSING BW-MINS325 is a packaged CAN-bus miniature inertial navigation system for unmanned aircraft, robotics and vehicle integration. Its 60 × 59 × 29 mm enclosure combines gyroscope and accelerometer functions, accepts 9–36 V DC power, and provides specified dynamic and static attitude accuracy with temperature compensation.

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Model and product typeBW-MINS325 CAN-bus miniature inertial navigation system
Dynamic attitude accuracy0.3°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90°; roll ±180°
Heading retention accuracy0.1°/60s
Gyroscope resolution0.01°/sec

Product overview

The BWSENSING BW-MINS325 is a compact inertial navigation component for integration into unmanned aircraft, robotic systems and other mobile platforms. Its packaged architecture incorporates gyroscope and accelerometer functions, with CAN output for connection to the host system. The enclosure measures 60 mm long, 59 mm wide and 29 mm high, defining the physical space needed for the unit. Electrical integration requires a 9–36 V DC supply, while temperature compensation accompanies its specified operating range of -40°C to +85°C.

Attitude performance distinguishes 0.3° dynamic accuracy from 0.01° static accuracy, with pitch measurement extending to ±90° and roll to ±180°. Heading retention is specified as 0.1° over 60 seconds. Kalman filtering and a dedicated bias-tracking algorithm support its inertial processing. The accelerometer covers ±1.8 g on each of three axes; its bias-stability figures apply at 25°C and differ with the stated measurement interval. The product configuration is a packaged sensing unit for host-platform integration, with applications also encompassing marine vehicles and platform stabilization.

Specifications

SpecificationValue & conditions
Model and product typeBW-MINS325 CAN-bus miniature inertial navigation system
Dynamic attitude accuracy0.3°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90°; roll ±180°
Heading retention accuracy0.1°/60s
Gyroscope resolution0.01°/sec
Gyroscope bias stability15°/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 100s0.001 mg25°C, 100s, 1σ.
Accelerometer bias stability at 10s0.01 mg25°C, 10s, 1σ.
Supply voltage9–36 V DC
Output interfaceCAN
Temperature range-40°C to +85°CTemperature compensated.
Dimensions60 × 59 × 29 mmPackaged product; length × width × height.
Bias trackingSpecial bias-tracking algorithm for drift elimination
FilteringHigh-performance Kalman filtering algorithm
Intended applicationsUnmanned surface vessels and underwater vehicles; robots; platform stabilization; large ships; automated guided vehicles; automated and unmanned driving; special-purpose vehicles; unmanned aircraft
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