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BW-AH325

By Wuxi Beiwei Sensing Technology ↗

The Wuxi Beiwei Sensing Technology BW-AH325 is a compact CAN-bus attitude and heading reference system for unmanned aircraft, robotics and platform stabilization. It includes gyroscope and accelerometer sensing, with 0.5° heading accuracy and 0.3° roll/pitch accuracy. The unit measures 60 × 59 × 29 mm and weighs 280g including its cable.

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Product identityBW-AH325 CAN-bus attitude and heading reference system
ManufacturerWuxi Beiwei Sensing Technology
Output interfaceCAN
Roll and pitch accuracy0.3°
Heading accuracy0.5°
Tilt rangePitch ±90º; roll ±180º

Product overview

The Wuxi Beiwei Sensing Technology BW-AH325 is an attitude and heading reference component for unmanned aircraft, unmanned vehicles, platform stabilization and robotic applications. Its architecture includes a gyroscope and a three-axis accelerometer, with CAN output. Roll and pitch accuracy is 0.3°, while heading accuracy is 0.5°. The tilt range covers pitch ±90º and roll ±180º. Gyroscope specifications include a ±400°/sec measurement range, 0.01°/sec resolution and 100Hz bandwidth; the accelerometer range is ±3.6 g on each of its X, Y and Z axes.

Mechanical integration requires space for a unit measuring L60 × W59 × H29 mm, with a weight of 280g including its cable. The BW-AH325 is a sensing component rather than a flight platform or airframe kit. It has temperature compensation over a -40℃ to +85℃ range and shock resistance of 2000g for 0.5ms, three shocks per axis. Measurement conditions matter: accelerometer bias stability at 25℃ and 1σ is 0.001mg over 100s or 0.01mg over 10s. Gyroscope bias stability across the full temperature range is 15°/h at 10s and 1σ.

Specifications

SpecificationValue & conditions
Product identityBW-AH325 CAN-bus attitude and heading reference system
ManufacturerWuxi Beiwei Sensing Technology
Output interfaceCAN
Roll and pitch accuracy0.3°
Heading accuracy0.5°
Tilt rangePitch ±90º; roll ±180º
Gyroscope resolution0.01°/sec
Gyroscope measurement range±400°/sec
Gyroscope bias stability15°/hAcross the full temperature range; 10s, 1σ.
Gyroscope angular random walk coefficientLess than 0.1 °/√h
Gyroscope scale factor nonlinearity≤100ppm1σ.
Gyroscope scale factor repeatability≤100ppm1σ.
Gyroscope bandwidth100Hz
Accelerometer measurement range±3.6 gX, Y and Z axes.
Accelerometer bias stability at 100 seconds0.001mg25℃, 100s, 1σ.
Accelerometer bias stability at 10 seconds0.01mg25℃, 10s, 1σ.
Temperature range-40℃ to +85℃Temperature compensated.
External dimensionsL60 × W59 × H29 mm
Weight280gIncluding cable.
Mean time between failures≥90000 hours
Electromagnetic compatibilityAccording to GBT17626
Insulation resistance≥100 MΩ
Shock resistance2000g0.5ms; 3 shocks per axis.
Application areasSatellite tracking; unmanned vehicles; platform stabilization; underwater robots; drilling equipment measurement and control; marine survey instruments; robot control; unmanned aircraft
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