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BW-MINS127

By BWSENSING ↗

The BWSENSING BW-MINS127 is a compact micro inertial navigation system for UAVs, robots, marine vehicles and platform stabilization. Gyroscope and accelerometer sensing combine with Kalman filtering and bias tracking. The packaged unit measures 60 × 59 × 29 mm, weighs 280 g including cable, and accepts 9–36V DC power with selectable communication outputs.

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Product identity and typeBWSENSING BW-MINS127 low-cost micro inertial navigation system with Modbus protocol
Dynamic accuracy1°
Static accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.5°/60s
Gyroscope resolution0.01°/sec

Product overview

The BWSENSING BW-MINS127 is a low-cost micro inertial navigation system intended for UAVs, robots, platform stabilization and other mobile applications. It combines gyroscope and accelerometer sensing with Kalman filtering and a special bias-tracking algorithm for drift elimination. The packaged unit measures 60 mm long, 59 mm wide and 29 mm high, with a weight of 280 g including its cable. Electrical integration uses a 9–36V DC supply, and selectable output options comprise RS232, RS485, TTL and Modbus.

The BW-MINS127 provides 1° dynamic accuracy and 0.01° static accuracy, with pitch measurement spanning ±90º and roll measurement spanning ±180º. Heading retention accuracy is 0.5°/60s, and the three-axis accelerometer range is ±1.8 g. Its temperature range is −40°C to +85°C with temperature compensation. Gyroscope bias stability across the full temperature range is 30°/h at 10s and 1σ. Shock resistance is 2000g for 0.5ms, with three shocks per axis; mean time between failures is at least 90,000 hours.

Specifications

SpecificationValue & conditions
Product identity and typeBWSENSING BW-MINS127 low-cost micro inertial navigation system with Modbus protocol
Dynamic accuracy1°
Static accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.5°/60s
Gyroscope resolution0.01°/sec
Gyroscope bias stability30°/hFull temperature range; 10s, 1σ.
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 100s0.001mg25°C, 100s, 1σ.
Accelerometer bias stability at 10s0.01mg25°C, 10s, 1σ.
Mean time between failures≥90,000 hours
Shock resistance2000g0.5ms; 3 shocks per axis.
Weight280gIncluding cable.
DimensionsL60 × W59 × H29 mmPackaged product.
Supply voltage9–36V DC
Interface optionsRS232 / RS485 / TTL / ModbusSelectable interface outputs.
Temperature range−40°C to +85°CWith temperature compensation.
Bias trackingSpecial bias-tracking algorithm for drift elimination
FilteringHigh-performance Kalman filtering algorithm
Application areasUncrewed boats and underwater vehicles; robots; platform stabilization; large vessels; automated guided vehicles; automated and driverless operation; special-purpose vehicles; UAVs
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