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BW-MINS427

By BWSENSING ↗

The BWSENSING BW-MINS427 is a compact, packaged micro inertial navigation system for unmanned aircraft, robotics and vehicle integration. It combines gyroscope and accelerometer sensing with Kalman filtering and bias tracking. Its 60 × 59 × 29 mm housing, 9–36 V DC supply and selectable serial or Modbus outputs define its principal integration requirements.

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ProductBWSENSING BW-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 holding accuracy0.1°/min
Gyroscope resolution0.01°/sec

Product overview

The BWSENSING BW-MINS427 is a packaged micro inertial navigation system for integration into unmanned aircraft and other moving platforms. Its physical envelope measures 60 mm long, 59 mm wide and 29 mm high, providing a compact component footprint for equipment integration. The system combines gyroscope and accelerometer measurement capabilities with Kalman filtering and bias tracking for drift control. Its application scope also includes robots, platform stabilization, unmanned boats, underwater vehicles, large ships and automated guided vehicles.

Electrical integration uses a 9–36 V DC supply, with selectable RS232, RS485, TTL or Modbus output. The temperature-compensated operating range extends from -40°C to +85°C. Attitude accuracy is 0.2° dynamically and 0.01° statically, with pitch coverage of ±90° and roll coverage of ±180°. Heading holding accuracy is 0.1°/min. The accelerometer range is ±1.8 g on each axis; its bias-stability figures depend on the specified temperature and averaging interval, while gyroscope bias stability is specified across the full temperature range.

Specifications

SpecificationValue & conditions
ProductBWSENSING BW-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 holding accuracy0.1°/min
Gyroscope resolution0.01°/sec
Gyroscope bias stability10°/hAcross the full 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 s0.001 mg25°C, 100 s, 1σ.
Accelerometer bias stability at 10 s0.01 mg25°C, 10 s, 1σ.
Supply voltage9–36 V DC
Interface optionsRS232 / RS485 / TTL / ModbusSelectable interface output.
Temperature range-40°C to +85°CTemperature compensated.
DimensionsL60 × W59 × H29 mmPackaged product.
Bias processingSpecial bias-tracking algorithm for drift elimination
FilteringHigh-performance Kalman filtering algorithm
ApplicationsUnmanned boats and underwater vehicles; robots; platform stabilization; large ships; automated guided vehicles; automated and unmanned driving; special-purpose vehicles; unmanned aircraft
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