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BW-MINS327

By Wuxi Beiwei Sensing Technology ↗

The Wuxi Beiwei Sensing Technology BW-MINS327 is a compact micro inertial navigation system for unmanned aircraft, robotics, vehicles and marine applications. Its 60 × 59 × 29 mm package provides gyroscope and accelerometer functions, Kalman filtering, selectable communication outputs, 9–36V DC power and temperature compensation.

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ManufacturerWuxi Beiwei Sensing Technology
Model and product typeBW-MINS327 micro inertial navigation system with Modbus protocol
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-MINS327 is a micro inertial navigation system for applications including unmanned aircraft, robots, platform stabilization and marine equipment. Its packaged dimensions are 60 mm long, 59 mm wide and 29 mm high, establishing the space needed for the instrument. Electrical integration requires a 9–36V DC supply, while output options include RS232, RS485, TTL and Modbus. The system incorporates gyroscope and accelerometer functions, Kalman filtering and a special bias-tracking algorithm for drift elimination.

Attitude measurement covers pitch of ±90° and roll of ±180°, with dynamic accuracy of 0.3° and static accuracy of 0.01°. Heading retention accuracy is 0.1°/60s. The gyroscope has 0.01°/sec resolution and full-temperature bias stability of 15°/h at 10s, 1σ. Acceleration measurement spans ±1.8 g on X, Y and Z. Accelerometer bias stability is 0.001mg at 100s and 0.01mg at 10s, both at 25°C and 1σ. The temperature range is -40°C to +85°C, with temperature compensation.

Specifications

SpecificationValue & conditions
ManufacturerWuxi Beiwei Sensing Technology
Model and product typeBW-MINS327 micro inertial navigation system with Modbus protocol
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 100 seconds0.001mg25°C, 100s, 1σ.
Accelerometer bias stability at 10 seconds0.01mg25°C, 10s, 1σ.
Supply voltage9–36V DC
Output optionsRS232 / RS485 / TTL / ModbusSelectable interface outputs.
Temperature range-40°C to +85°CTemperature compensated.
DimensionsL60 × W59 × H29 mmPackaged product.
Bias trackingSpecial bias-tracking algorithm for drift elimination
FilteringHigh-performance Kalman filtering algorithm
Application areasUnmanned boats and underwater vehicles; robots; platform stabilization; large vessels; automated guided vehicles; automated and driverless operation; special-purpose vehicles; unmanned aircraft
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