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BW-MINS325E

By Wuxi Beiwei Sensing Technology ↗

The Wuxi Beiwei Sensing Technology BW-MINS325E is a CAN-bus micro inertial navigation component for unmanned aircraft, robotic vehicles and stabilization systems. Packaged and bare-board formats support integration into larger equipment. It combines attitude measurement, heading retention and output up to 500Hz with 9-36V DC power and temperature-compensated operation.

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Product identityBW-MINS325E CAN-bus micro inertial navigation system
Supply voltage9-36V DC
Operating current30mA; 40mA maximum
Operating temperature-40 to 85°C
Storage temperature-55 to 100°C
Dynamic attitude accuracy0.3°

Product overview

The Wuxi Beiwei Sensing Technology BW-MINS325E provides inertial attitude measurement for integration into unmanned aircraft and other mobile or stabilized systems. Its CAN interface supports connection to a host system, with a maximum output frequency of 500Hz. Attitude specifications distinguish 0.3° dynamic accuracy from 0.01° static accuracy, while the measurement envelope covers pitch through ±90° and roll through ±180°. Heading retention is specified separately at 0.1°/60s, giving integrators a time-based heading parameter alongside the attitude measurements.

Physical integration options comprise a packaged unit measuring 97 × 63 × 27.2 mm and a bare-board format measuring 60 × 54 × 6 mm. The bare board’s length and width may vary by ±1mm, so installation space must accommodate that qualification. Weight is 280g including the cable. This is an inertial navigation component for incorporation into a larger system; its described configurations are the packaged sensor and bare board, rather than a flight platform or airframe kit.

Electrical integration requires a 9-36V DC supply, with operating current of 30mA and a 40mA maximum. Temperature compensation accompanies an operating range of -40 to 85°C; storage extends from -55 to 100°C. Environmental specifications include electromagnetic compatibility in accordance with GBT17626, insulation resistance of at least 100 MΩ, and shock resistance of 2000g for 0.5ms, applied three times per axis. The mean time between failures is specified as at least 90,000 hours.

Specifications

SpecificationValue & conditions
Product identityBW-MINS325E CAN-bus micro inertial navigation system
Supply voltage9-36V DC
Operating current30mA; 40mA maximum
Operating temperature-40 to 85°C
Storage temperature-55 to 100°C
Dynamic attitude accuracy0.3°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90°; roll ±180°
Heading retention accuracy0.1°/60s
Communication interfaceCAN
Maximum output frequency500Hz
Mean time between failures≥90,000 hours per failure
Electromagnetic compatibilityIn accordance with GBT17626
Insulation resistance≥100 MΩ
Shock resistance2000g0.5ms pulse duration; 3 shocks per axis.
Weight280gIncluding cable.
Packaged dimensionsL97 × W63 × H27.2 mmPackaged product.
Bare-board dimensionsL60 × W54 × H6 mmBare-board product; length and width may vary by ±1mm, with actual dimensions governing.
Temperature compensationTemperature compensated
Application areasUnmanned boats and underwater vehicles; robots; platform stabilization; large ships; automated guided vehicles; automated and autonomous driving; special-purpose vehicles; unmanned aircraft
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