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BW-MINS200

By BWSENSING ↗

The BWSENSING BW-MINS200 is a miniature inertial navigation system for unmanned aircraft, robotics, vehicles and platform stabilization. Its packaged dimensions are 60 × 59 × 29 mm, with selectable RS232, RS485 or TTL output. Attitude accuracy is 0.5° dynamically and 0.01° statically.

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Model and product typeBW-MINS200 miniature inertial navigation system
Dynamic attitude accuracy0.5°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.3°/60s
Gyroscope resolution0.01°/sec

Product overview

The BWSENSING BW-MINS200 is a miniature inertial navigation system intended for unmanned aircraft, robots, platform stabilization and vehicle applications. Its packaged dimensions are 60 mm long, 59 mm wide and 29 mm high, providing a compact physical envelope for integration. Output options are RS232, RS485 or TTL, with the interface selectable for the installation. Its sensing specifications cover a gyroscope and an accelerometer with measurement on the X, Y and Z axes; processing includes Kalman filtering and a special bias-tracking algorithm for drift elimination.

Dynamic attitude accuracy is 0.5°, while static accuracy is 0.01°. The attitude measurement range covers pitch to ±90º and roll to ±180º, with heading retention accuracy of 0.3°/60s. The accelerometer range is ±1.8 g on each axis. Its bias stability is 0.001mg at 25°C over 100s and 0.01mg at 25°C over 10s, both at 1σ. Gyroscope bias stability across the full temperature range is 20°/h under the stated 10s, 1σ condition, and angular random walk is below 0.1 °/√h.

Specifications

SpecificationValue & conditions
Model and product typeBW-MINS200 miniature inertial navigation system
Dynamic attitude accuracy0.5°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.3°/60s
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 100s0.001mg25°C, 100s, 1σ.
Accelerometer bias stability at 10s0.01mg25°C, 10s, 1σ.
DimensionsL60 × W59 × H29 mmPackaged product.
Output interface optionsRS232, RS485 or TTLSelectable output interface.
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 driverless driving; special-purpose vehicles; unmanned aircraft
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