BW-MINS200
By BWSENSINGThe BWSENSING BW-MINS200 is a miniature inertial navigation system for unmanned aircraft, robotics, vehicles and platform stabilization. Its packaged dimensions are 60 × 59 × 29 mm, with selectable RS232, RS485 or TTL output. Attitude accuracy is 0.5° dynamically and 0.01° statically.
Explore product ↗industryBW-MINS225
By BWSENSINGThe 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.
Explore product ↗industryBW-MINS225E
By BWSENSINGThe BWSENSING BW-MINS225E is a low-cost miniature inertial navigation system for integration into UAVs, robots and stabilized platforms. It combines CAN communication, Kalman filtering and temperature compensation. Packaged and bare-board dimensions support installation planning, while key specifications include 0.5° dynamic attitude accuracy, 0.3°/60s heading retention accuracy and a 500Hz maximum output frequency.
Explore product ↗industryBW-MINS300
By BWSENSINGThe BWSENSING BW-MINS300 is a compact micro inertial navigation unit for unmanned aircraft, robotics, marine vehicles and platform stabilization. It features gyroscope and three-axis accelerometer sensing, Kalman filtering, selectable serial outputs and a 9–36 V DC supply. Its body measures 60 × 59 × 29 mm.
Explore product ↗industryBW-MINS325
By BWSENSINGThe BWSENSING BW-MINS325 is a packaged CAN-bus miniature inertial navigation system for unmanned aircraft, robotics and vehicle integration. Its 60 × 59 × 29 mm enclosure combines gyroscope and accelerometer functions, accepts 9–36 V DC power, and provides specified dynamic and static attitude accuracy with temperature compensation.
Explore product ↗industryBW-MINS325E
By BWSENSINGThe BWSENSING BW-MINS325E is a CAN-bus micro inertial navigation system for attitude sensing and stabilization in unmanned aircraft and other mobile platforms. Packaged and bare-board configurations provide different installation envelopes. It combines a 9-36V DC supply range, output up to 500Hz, and specified static, dynamic and heading-hold accuracy.
Explore product ↗industryBW-MINS327
By BWSENSINGThe BWSENSING BW-MINS327 is a compact micro inertial navigation system for unmanned aircraft, robots, vehicles and stabilized platforms. Its 60 × 59 × 29 mm package provides gyroscope and accelerometer sensing, Kalman filtering and bias tracking, with a 9–36V DC supply and selectable interface outputs.
Explore product ↗industryBW-MINS400
By BWSENSINGThe BWSENSING BW-MINS400 is a compact micro inertial navigation unit for integration into unmanned aircraft and other mobile or stabilized systems. It combines gyroscope and three-axis accelerometer sensing in a 60 × 59 × 29 mm package, with selectable serial outputs, 9–36V DC power and temperature compensation.
Explore product ↗industryBW-MINS425
By BWSENSINGThe 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.
Explore product ↗industryBW-MINS427
By BWSENSINGThe BWSENSING BW-MINS427 is a compact, packaged micro inertial navigation system for unmanned aircraft, robotics and vehicle integration. It combines gyroscope and accelerometer sensing with Kalman filtering and bias tracking. Its 60 × 59 × 29 mm housing, 9–36 V DC supply and selectable serial or Modbus outputs define its principal integration requirements.
Explore product ↗industryBW-MINS500
By BWSENSINGThe BWSENSING BW-MINS500 is a miniature inertial navigation system for UAVs, robots, marine vehicles and stabilized platforms. It measures 60 × 59 × 29 mm, accepts 9–36 V DC and offers selectable RS232, RS485 or TTL outputs. Dynamic attitude accuracy is 0.1°, with static accuracy of 0.01° and temperature-compensated operation.
Explore product ↗industryBW-MINS525
By BWSENSINGThe BWSENSING BW-MINS525 is a packaged CAN-bus micro inertial navigation unit for unmanned aircraft, robotics and platform stabilization. Its 60 × 59 × 29 mm housing integrates gyroscope and accelerometer functions, with 9–36V DC power, temperature compensation and separate dynamic, static and heading-retention specifications.
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