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BW-MINS325

By Wuxi Beiwei Sensing Technology ↗

The Wuxi Beiwei Sensing Technology BW-MINS325 is a compact CAN-bus micro inertial navigation unit for integration into unmanned aircraft and other mobile or stabilized systems. Its packaged configuration combines gyroscope and accelerometer functions, 9–36V DC power, temperature compensation, bias tracking and Kalman filtering in a 60 × 59 × 29 mm enclosure.

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ManufacturerWuxi Beiwei Sensing Technology
Model and product typeBW-MINS325 CAN-bus micro inertial navigation system
Dynamic attitude accuracy0.3°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90°; roll ±180°
Heading retention accuracy0.1°/60s

Product overview

The Wuxi Beiwei Sensing Technology BW-MINS325 is a packaged micro inertial navigation system with gyroscope and accelerometer functions, CAN output and a 9–36V DC supply input. Its 60 × 59 × 29 mm enclosure defines the space occupied by the sensing unit within a host installation. Intended applications include unmanned aircraft, unmanned boats, underwater vehicles, robots and platform stabilization. Its product configuration is an inertial navigation component for integration into these systems.

Attitude specifications distinguish 0.3° dynamic accuracy from 0.01° static accuracy, with pitch measurement to ±90° and roll to ±180°. Heading retention is specified at 0.1°/60s, while the accelerometer range is ±1.8 g on each axis. Bias tracking, Kalman filtering and temperature compensation support the sensing functions across a stated −40°C to +85°C temperature range. Accelerometer bias stability carries separate 10-second and 100-second qualifications at 25°C; gyroscope bias stability is specified across the full temperature range.

Specifications

SpecificationValue & conditions
ManufacturerWuxi Beiwei Sensing Technology
Model and product typeBW-MINS325 CAN-bus micro 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°/hAcross the full 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°C, 100s, 1σ.
Accelerometer bias stability over 10 seconds0.01mg25°C, 10s, 1σ.
DC supply voltage9–36V DC
Output interfaceCAN
Temperature range-40°C to +85°CTemperature compensated.
DimensionsL60 × W59 × H29 mmPackaged product.
Bias trackingSpecial bias-tracking algorithm for drift suppression
FilteringKalman filtering algorithm
ApplicationsUnmanned boats and underwater vehicles; robots; platform stabilization; large ships; automated guided vehicles; automated and driverless operation; special-purpose vehicles; unmanned aircraft
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