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BW-MINS500

By Wuxi Beiwei Sensing Technology ↗

The Wuxi Beiwei Sensing Technology BW-MINS500 is a compact micro inertial navigation system intended for unmanned aircraft, robotics and other vehicle or stabilization applications. Its 60 × 59 × 29 mm envelope, 9–36V DC supply and selectable serial interfaces support host-platform integration, with specified attitude accuracy, heading retention and temperature-qualified inertial sensor performance.

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Product identityWuxi Beiwei Sensing Technology BW-MINS500 ultra-high-precision micro inertial navigation system
Dynamic attitude accuracy0.1°
Static attitude accuracy0.01°
Heading retention accuracy0.1°/min
Gyroscope resolution0.01°/sec
Gyroscope bias stability5°/hAcross the full temperature range; 10s, 1σ.

Product overview

Wuxi Beiwei Sensing Technology’s BW-MINS500 is a compact micro inertial navigation system for integration into unmanned aircraft and other moving platforms. Its sensing specifications cover gyroscope and accelerometer performance, alongside attitude accuracy and heading retention. The unit occupies an external envelope of 60 × 59 × 29 mm and accepts 9–36V DC power. Selectable RS232, RS485 or TTL output provides interface choices for integration with the host platform’s electronics, with the interface selected as part of the configuration.

The BW-MINS500 specifies 0.1° dynamic attitude accuracy, 0.01° static accuracy and heading retention accuracy of 0.1°/min. It combines a bias-tracking algorithm for drift elimination with high-performance Kalman filtering and temperature compensation across -40℃ to +85℃. Gyroscope bias stability is 5°/h over the full temperature range under a 10-second, one-sigma condition. Accelerometer bias stability has separate qualifications: 0.001mg at 25℃ over 100 seconds and 0.01mg at 25℃ over 10 seconds, both at one sigma.

Specifications

SpecificationValue & conditions
Product identityWuxi Beiwei Sensing Technology BW-MINS500 ultra-high-precision micro inertial navigation system
Dynamic attitude accuracy0.1°
Static attitude accuracy0.01°
Heading retention accuracy0.1°/min
Gyroscope resolution0.01°/sec
Gyroscope bias stability5°/hAcross the full temperature range; 10s, 1σ.
Accelerometer bias stability at 100 seconds0.001mg25℃, 100s, 1σ.
Accelerometer bias stability at 10 seconds0.01mg25℃, 10s, 1σ.
Supply voltage9–36V DC
Output interface optionsRS232 / RS485 / TTLSelectable output interface.
Temperature range-40℃ to +85℃With temperature compensation.
External dimensionsL60 × W59 × H29 mm
Bias trackingSpecial bias-tracking algorithm for drift elimination
FilteringHigh-performance Kalman filtering algorithm
Application areasUnmanned 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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