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BW-MINS127

By Wuxi Beiwei Sensing Technology ↗

Wuxi Beiwei Sensing Technology’s BW-MINS127 is a compact micro inertial navigation system for integration into unmanned aircraft and other mobile or stabilized platforms. It combines gyroscope and accelerometer sensing with Kalman filtering, selectable communication outputs and a 9–36 V DC supply. Its packaged dimensions are 60 × 59 × 29 mm, with a cable-inclusive weight of 280 g.

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ManufacturerWuxi Beiwei Sensing Technology
Model and product typeBW-MINS127 low-cost micro inertial navigation system with Modbus protocol
Dynamic attitude accuracy1°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.5°/60s

Product overview

The BW-MINS127 from Wuxi Beiwei Sensing Technology is a low-cost micro inertial navigation system intended for applications including unmanned aircraft, robots, platform stabilization, unmanned boats and underwater vehicles. Its sensing architecture includes gyroscope and accelerometer functions, supported by Kalman filtering and a dedicated bias-tracking algorithm for drift elimination. Attitude specifications distinguish 1° dynamic accuracy from 0.01° static accuracy, with pitch coverage of ±90º and roll coverage of ±180º. Heading retention accuracy is specified as 0.5°/60s.

The packaged unit measures 60 × 59 × 29 mm and weighs 280 g including its cable, providing concrete space and mass requirements for integration. It accepts 9–36 V DC and offers selectable RS232, RS485, TTL and Modbus output options. Temperature compensation accompanies a −40°C to +85°C temperature range. Integration must also account for the accelerometer’s ±1.8 g range on each axis and the separately specified shock resistance of 2000g for 0.5 ms, three times per axis.

Specifications

SpecificationValue & conditions
ManufacturerWuxi Beiwei Sensing Technology
Model and product typeBW-MINS127 low-cost micro inertial navigation system with Modbus protocol
Dynamic attitude accuracy1°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.5°/60s
Gyroscope resolution0.01°/sec
Gyroscope bias stability over temperature30°/h10s, 1σ; full temperature range.
Gyroscope angular random walk coefficientLess than 0.1 °/√h
Gyroscope bias repeatabilityLess than 50 °/h1σ.
Accelerometer range±1.8 gX, Y and Z axes.
Accelerometer bias stability at 100s0.001 mg25°C, 100s, 1σ.
Accelerometer bias stability at 10s0.01 mg25°C, 10s, 1σ.
Mean time between failures≥90,000 hours
Shock resistance2000g0.5 ms; 3 shocks per axis.
Weight280 gIncluding cable.
DimensionsL60 × W59 × H29 mmPackaged product.
Supply voltage9–36 V DCDC supply.
Temperature range and compensation−40°C to +85°C; temperature compensation
Interfaces and protocolRS232 / RS485 / TTL / ModbusSelectable output options.
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 unmanned driving; special-purpose vehicles; unmanned aircraft
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