ChinaDrone.Request a quote ↗
COMPONENT

BW-MINS425

By BWSENSING ↗

The BWSENSING BW-MINS425 is a compact CAN-bus inertial navigation component for unmanned aircraft, robotics, vehicles and platform stabilization. Its 60 × 59 × 29 mm package combines gyroscope and accelerometer sensing, Kalman filtering and bias tracking, with 9–36VDC power and temperature compensation from −40°C to +85°C.

Request a quote ↗
Product identity and typeBWSENSING BW-MINS425 high-precision CAN-bus miniature inertial navigation system
Dynamic accuracy0.2°
Static accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.1°/min
Gyroscope resolution0.01°/sec

Product overview

The BWSENSING BW-MINS425 is a miniature inertial navigation system for integration into unmanned aircraft, robotic systems and other vehicle or stabilization applications. Its packaged body measures 60 mm long, 59 mm wide and 29 mm high, defining the component’s installation envelope. The hardware combines gyroscope and accelerometer measurements with CAN output, a 9–36VDC supply input and temperature compensation across −40°C to +85°C. This configuration provides a compact inertial sensing component for a larger integrated system.

Attitude performance includes 0.2° dynamic accuracy and 0.01° static accuracy, with pitch measurement spanning ±90º and roll spanning ±180º. Heading retention accuracy is 0.1°/min. Processing includes Kalman filtering and a dedicated bias-tracking algorithm for drift elimination. The accelerometer range is ±1.8 g on each of three axes. Its bias-stability figures have distinct measurement conditions: 0.001mg at 25°C over 100 seconds and 0.01mg at 25°C over 10 seconds, both at 1σ. Gyroscope full-temperature bias stability is 10°/h at 10 seconds, 1σ.

Specifications

SpecificationValue & conditions
Product identity and typeBWSENSING BW-MINS425 high-precision CAN-bus miniature inertial navigation system
Dynamic accuracy0.2°
Static accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.1°/min
Gyroscope resolution0.01°/sec
Gyroscope bias stability10°/hAcross the full temperature range; 10s, 1σ.
Angular random walk coefficientLess than 0.1 °/√h
Accelerometer measurement 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.
Supply voltage9–36VDC
Output interfaceCAN
Temperature range and compensation-40°C to +85°C; temperature compensation
DimensionsL60 × W59 × H29 mmPackaged product.
Bias trackingDedicated 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
SOURCE WITH CHINADRONE

Request a quote for BW-MINS425

Send your application, destination country and expected quantity to the ChinaDrone team. We can discuss product selection, configuration and sourcing from China.

Submit your procurement requirements ↗

No account needed. A model number is optional. Your enquiry is handled by ChinaDrone.

KEEP EXPLORING

Similar products

Browse all products ↗
GEPRC CEP-STABLE 12A Whoop Stack with stacked circuit boards and mounting hardware
Flight control & navigation

CEP-STABLE 12A Whoop Stack

By GEPRC

The GEPRC CEP-STABLE 12A Whoop Stack is an electronics package for small indoor Whoop and toothpick UAV builds. It combines F4 flight control, 12A ESC capability and a selectable-power 5.8GHz video transmitter. Its 2–4S LiPo support, compact M2 mounting pattern and supplied installation hardware suit integration into a separately assembled aircraft.

Flight control & navigation

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℃.

Flight control & navigation

BW-MINS225

By BWSENSING

The BWSENSING BW-MINS225 is a compact CAN bus miniature inertial navigation system for integration into unmanned aircraft and other mobile or stabilized equipment. Its 60 × 59 × 29 mm package provides gyroscope and accelerometer functions, temperature compensation, bias tracking and Kalman filtering, with 9–36V DC power and a -40℃ to +85℃ temperature range.

Bynav Gmouse module-integrated RTK antenna shown from below with mounting hardware.
Flight control & navigation

Bynav Gmouse Module-integrated RTK Antenna

By Bynav

The bynav Gmouse Module-integrated RTK Antenna is an integrated GNSS/INS positioning component for machinery and unmanned-system integration. Its Gmouse-M20, M21 and M22 configurations combine an M2-series module with antenna hardware; built-in positioning electronics and inertial sensing support high-precision navigation, with configuration-dependent output rates and qualified accuracy specifications.