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BW-MINS100

By BWSENSING ↗

The BWSENSING BW-MINS100 is a compact micro inertial navigation system for integration into UAVs, vehicles, marine equipment and stabilized platforms. Its packaged gyroscope and accelerometer functions occupy 60 × 59 × 29 mm. It supports selectable serial interfaces, 9–36V DC power and temperature-compensated operation from −40℃ to +85℃.

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Product identity and typeBWSENSING BW-MINS100 micro inertial navigation system
Packaged dimensionsL60 × W59 × H29 mm
Dynamic attitude accuracy1°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.5°/60s

Product overview

The BWSENSING BW-MINS100 provides inertial sensing for unmanned aircraft and other mobile or stabilized equipment. Its packaged architecture combines gyroscope and accelerometer functions within a 60 × 59 × 29 mm envelope, giving integrators a defined space requirement for installation. It is an instrumentation component for integration into a host system. Intended uses also include unmanned boats, underwater vehicles, robotics, platform stabilization, large vessels, automated guided vehicles and special-purpose vehicles.

Electrical integration requires a 9–36V DC supply, with RS232, RS485 or TTL available as selectable output interfaces. The system incorporates Kalman filtering, dedicated bias tracking and temperature compensation across −40℃ to +85℃. Attitude specifications distinguish 1° dynamic accuracy from 0.01° static accuracy, with pitch coverage of ±90º and roll coverage of ±180º. Heading retention is specified as 0.5°/60s, while accelerometer bias-stability figures depend on the stated temperature, observation interval and statistical qualification.

Specifications

SpecificationValue & conditions
Product identity and typeBWSENSING BW-MINS100 micro inertial navigation system
Packaged dimensionsL60 × W59 × H29 mm
Dynamic attitude accuracy1°
Static attitude 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
Accelerometer 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.
Power supply9–36V DC
Interface optionsRS232, RS485 or TTLSelectable output interface.
Temperature range-40℃ to +85℃Temperature compensated.
Bias trackingDedicated bias-tracking algorithm for drift elimination
FilteringKalman filtering algorithm
Intended applicationsUnmanned boats, underwater vehicles, robots, platform stabilization, large vessels, automated guided vehicles, automated and driverless operation, special-purpose vehicles, and unmanned aircraft
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