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BW-MINS427

By Wuxi Beiwei Sensing Technology ↗

The Wuxi Beiwei Sensing Technology BW-MINS427 is a high-precision micro inertial navigation system for UAVs, other unmanned vehicles and stabilization applications. The 60 × 59 × 29 mm packaged unit provides attitude, gyroscope and accelerometer measurements, selectable communications outputs, 9–36 V DC power input and temperature compensation.

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Product typeBW-MINS427 high-precision micro inertial navigation system with Modbus protocol.
Dynamic attitude accuracy0.2°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90°; roll ±180.
Heading retention accuracy0.1°/min
Gyroscope resolution0.01°/sec

Product overview

The BW-MINS427 is a packaged micro inertial navigation unit with attitude, gyroscope and accelerometer specifications. Its enclosure measures 60 mm long, 59 mm wide and 29 mm high. Electrical integration uses a 9–36 V DC supply, with selectable RS232, RS485, TTL and Modbus output options. Intended applications include UAVs, unmanned boats, underwater vehicles, robots and platform stabilization, as well as large vessels, automated guided vehicles, automated and unmanned driving, and special-purpose vehicles.

Dynamic attitude accuracy is 0.2°, static accuracy is 0.01°, and heading retention accuracy is 0.1°/min. The pitch measurement range is ±90°, while the accelerometer range is ±1.8 g on each of its three axes. The unit features temperature compensation across -40°C to +85°C, Kalman filtering and a dedicated bias-tracking algorithm. Accelerometer bias stability is 0.001 mg over 100 seconds and 0.01 mg over 10 seconds, both at 25°C and 1σ; gyroscope full-temperature bias stability is 10°/h under a 10-second, 1σ condition.

Specifications

SpecificationValue & conditions
Product typeBW-MINS427 high-precision micro inertial navigation system with Modbus protocol.
Dynamic attitude accuracy0.2°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90°; roll ±180.
Heading retention accuracy0.1°/min
Gyroscope resolution0.01°/sec
Gyroscope bias stability10°/hFull temperature range; 10 s, 1σ.
Angular random walk coefficientLess than 0.1 °/√h
Accelerometer range±1.8 gX, Y and Z axes.
Accelerometer bias stability at 100 seconds0.001 mg25°C, 100 s, 1σ.
Accelerometer bias stability at 10 seconds0.01 mg25°C, 10 s, 1σ.
Packaged dimensionsL60 × W59 × H29 mm
Supply voltage9–36 V DC
Interface optionsRS232 / RS485 / TTL / ModbusSelectable interface output.
Temperature range-40°C to +85°CTemperature compensated.
Bias trackingSpecial bias-tracking algorithm for drift elimination.
FilteringHigh-performance Kalman filtering algorithm.
Intended applicationsUnmanned boats and underwater vehicles, robots, platform stabilization, large vessels, automated guided vehicles, automated and unmanned driving, special-purpose vehicles, and UAVs.
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