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BW-MINS100

By Wuxi Beiwei Sensing Technology ↗

The Beiwei Sensing BW-MINS100 is a compact micro inertial navigation system for unmanned aircraft and other mobile or stabilized platforms. Its 60 × 59 × 29 mm package combines attitude, gyroscope and accelerometer sensing specifications with selectable serial outputs, 9–36V DC power and temperature compensation.

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Manufacturer and modelBeiwei Sensing BW-MINS100 micro inertial navigation system
Dynamic attitude accuracy1°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.5°/60s60-second interval.
Gyroscope resolution0.01°/sec

Product overview

The Beiwei Sensing BW-MINS100 is a packaged micro inertial navigation system for integration into unmanned aircraft, robots, marine vehicles and stabilization platforms. Its sensing specification covers attitude, gyroscope and accelerometer parameters, with pitch measurement to ±90º and roll measurement to ±180º. The package measures 60 mm long, 59 mm wide and 29 mm high, defining its physical integration envelope. Electrical integration uses a 9–36V DC supply, with selectable RS232, RS485 or TTL output.

The system combines a bias-tracking algorithm for drift elimination with Kalman filtering and temperature compensation across -40°C to +85°C. Static attitude accuracy is 0.01°, while dynamic accuracy is 1°; heading retention accuracy is 0.5° over 60 seconds. Gyroscope bias stability is 30°/h across the full temperature range under the 10-second, 1σ qualification. Accelerometer bias stability is specified separately at 25°C for 100-second and 10-second intervals, so those figures retain distinct measurement conditions.

Specifications

SpecificationValue & conditions
Manufacturer and modelBeiwei Sensing BW-MINS100 micro inertial navigation system
Dynamic attitude accuracy1°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.5°/60s60-second interval.
Gyroscope resolution0.01°/sec
Gyroscope bias stability30°/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 over 100 seconds0.001mg25°C, 100s, 1σ.
Accelerometer bias stability over 10 seconds0.01mg25°C, 10s, 1σ.
Supply voltage9–36V DC
Interface optionsRS232, RS485 or TTLSelectable output interface.
Temperature range-40°C to +85°CTemperature compensated.
DimensionsL60 × W59 × H29 mmPackaged product.
Bias trackingSpecial bias-tracking algorithm for drift elimination
FilteringHigh-performance Kalman filtering algorithm
Application areasUnmanned boats and underwater vehicles; robots; platform stabilization; large ships; automated guided vehicles; automated and driverless driving; special-purpose vehicles; unmanned aircraft
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