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BW-MINS200

By Wuxi Beiwei Sensing Technology ↗

The Wuxi Beiwei Sensing Technology BW-MINS200 is a compact micro inertial navigation system for unmanned aircraft and other mobile or stabilized equipment. Its 60 × 59 × 29 mm package offers selectable RS232, RS485 or TTL output, Kalman filtering, and specified attitude, gyroscope and three-axis accelerometer performance.

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ManufacturerWuxi Beiwei Sensing Technology
Model and product typeBW-MINS200 micro inertial navigation system
Dynamic attitude accuracy0.5°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.3°/60sOver 60 seconds.

Product overview

The Wuxi Beiwei Sensing Technology BW-MINS200 is a micro inertial navigation system intended for integration into unmanned aircraft, robots, marine vehicles and stabilization platforms. Its packaged body measures 60 mm long, 59 mm wide and 29 mm high, defining the space occupied by the unit. Its sensing specifications cover gyroscope performance and acceleration measurement on the X, Y and Z axes. Output interface choices are RS232, RS485 or TTL, providing selectable electrical integration options.

The BW-MINS200 combines Kalman filtering with a special bias tracking algorithm for drift elimination. Its attitude specifications distinguish 0.5° dynamic accuracy from 0.01° static accuracy, with pitch measurement limited to ±90º and roll to ±180º. Heading retention is specified as 0.3° over 60 seconds. The accelerometer range is ±1.8 g on each axis, while its two bias stability values apply at 25℃ with different measurement durations; those conditions matter when comparing integration requirements.

Specifications

SpecificationValue & conditions
ManufacturerWuxi Beiwei Sensing Technology
Model and product typeBW-MINS200 micro inertial navigation system
Dynamic attitude accuracy0.5°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.3°/60sOver 60 seconds.
Gyroscope resolution0.01°/sec
Gyroscope bias stability20°/hFull temperature range; 10s, 1σ.
Angular random walk coefficientLess than 0.1 °/√h
Accelerometer range±1.8 gX, Y and Z axes.
Accelerometer bias stability at 100 seconds0.001mg25℃, 100s, 1σ.
Accelerometer bias stability at 10 seconds0.01mg25℃, 10s, 1σ.
Packaged dimensionsL60 × W59 × H29 mm
Interface optionsRS232, RS485 or TTLSelectable output interface.
Drift compensationSpecial bias tracking algorithm for drift elimination
FilteringHigh-performance Kalman filtering algorithm
ApplicationsUnmanned 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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