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BW-MINS400

By BWSENSING ↗

The BWSENSING BW-MINS400 is a compact micro inertial navigation unit for integration into unmanned aircraft and other mobile or stabilized systems. It combines gyroscope and three-axis accelerometer sensing in a 60 × 59 × 29 mm package, with selectable serial outputs, 9–36V DC power and temperature compensation.

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Product identity and typeBWSENSING BW-MINS400 high-precision micro inertial navigation unit
Dynamic accuracy0.2°
Static accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.1°/min
Gyroscope resolution0.01°/sec

Product overview

The BWSENSING BW-MINS400 is a packaged micro inertial navigation unit for applications including unmanned aircraft, robots, unmanned boats and underwater vehicles, platform stabilization, and automated guided vehicles. Its sensing architecture includes a gyroscope and a three-axis accelerometer, with Kalman filtering and a dedicated bias-tracking algorithm for drift elimination. The enclosure measures 60 mm long, 59 mm wide and 29 mm high, defining the physical space required for the unit within a host system.

Electrical integration uses a 9–36V DC supply and a selectable RS232, RS485 or TTL output interface. The temperature range is -40℃ to +85℃ with temperature compensation. Attitude measurement covers pitch to ±90º and roll to ±180º, with dynamic accuracy of 0.2° and static accuracy of 0.01°. Heading retention accuracy is 0.1°/min. The accelerometer range is ±1.8 g on each axis; its two bias-stability figures apply specifically at 25℃ and use different measurement intervals.

Specifications

SpecificationValue & conditions
Product identity and typeBWSENSING BW-MINS400 high-precision micro inertial navigation unit
Dynamic accuracy0.2°
Static accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.1°/min
Gyroscope resolution0.01°/sec
Gyroscope bias stability10°/hAcross the full 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℃, 100s, 1σ.
Accelerometer bias stability at 10 seconds0.01mg25℃, 10s, 1σ.
Supply voltage9–36V DC
Interface optionsRS232, RS485 or TTLSelectable output interface.
Temperature range-40℃ to +85℃Temperature compensation.
Packaged dimensionsL60 × W59 × H29 mm
Bias trackingSpecial bias-tracking algorithm for drift elimination
FilteringHigh-performance Kalman filter algorithm
Application areasUnmanned boats and underwater vehicles; robots; platform stabilization; large vessels; automated guided vehicles; automated and unmanned driving; special-purpose vehicles; unmanned aircraft
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