ChinaDrone.Request a quote ↗
COMPONENT

BW-AH55

By BWSENSING ↗

The BWSENSING BW-AH55 is a low-cost CAN-interface attitude and heading reference system for UAVs and other equipment. Packaged and bare-board formats have distinct installation dimensions. It supports dynamic and static measurements, compensated processing and output up to 100Hz, using a 5-12V DC supply.

Request a quote ↗
Product typeBW-AH55 low-cost CAN-interface attitude and heading reference system
Supply voltage5-12V DC
Operating current30mA; 40mA maximum
Operating temperature-40 to 85°C
Storage temperature-55 to 100°C
Pitch accuracy3° RMS dynamic; 0.5° RMS staticRMS; dynamic and static measurement.

Product overview

The BWSENSING BW-AH55 is an attitude and heading reference system for integration into unmanned aircraft, robots, surveying instruments and other equipment. It supports dynamic and static measurements and incorporates CAN connectivity, a high-performance binary output protocol and Kalman filtering. Its processing features include gyroscope drift compensation, nonlinearity and orthogonality compensation, and a dedicated bias-tracking algorithm for drift elimination. Electrical integration uses a 5-12V DC supply, with operating current of 30mA and a maximum of 40mA. Maximum output frequency is 100Hz, startup delay is under three seconds, and serial communication rates span 2400 to 115200 baud.

Physical formats comprise a packaged unit measuring L55 × W37 × H24 mm and a bare board measuring L33 × W27 × H6 mm. Bare-board length and width may vary by ±1mm; actual dimensions govern. Pitch and roll accuracy is 3° RMS during dynamic measurement and 0.5° RMS during static measurement. Heading accuracy is 3°, with 0.01° resolution for both attitude and heading. Measurement ranges are ±90° in pitch and ±180° in roll. Operating temperature spans -40 to 85°C with temperature compensation, storage temperature spans -55 to 100°C, and shock resistance is 2000g.

Specifications

SpecificationValue & conditions
Product typeBW-AH55 low-cost CAN-interface attitude and heading reference system
Supply voltage5-12V DC
Operating current30mA; 40mA maximum
Operating temperature-40 to 85°C
Storage temperature-55 to 100°C
Pitch accuracy3° RMS dynamic; 0.5° RMS staticRMS; dynamic and static measurement.
Roll accuracy3° RMS dynamic; 0.5° RMS staticRMS; dynamic and static measurement.
Attitude resolution0.01°
Tilt rangePitch ±90°; roll ±180°
Heading accuracy3°
Heading resolution0.01°
Startup delayLess than 3s
Maximum output frequency100Hz
Serial communication rate2400 to 115200 baud
Digital output formatHigh-performance binary protocol
Shock resistance2000g
Packaged dimensionsL55 × W37 × H24 mmPackaged product.
Bare-board dimensionsL33 × W27 × H6 mmBare-board product; length and width may vary by ±1mm, with actual dimensions governing.
Measurement modesDynamic and static measurement
InterfaceCAN
Gyroscope compensationGyroscope drift compensation
Calibration compensationNonlinearity and orthogonality compensation
Bias trackingDedicated bias-tracking algorithm for drift elimination
Temperature compensationTemperature compensation-40°C to +85°C.
FilteringHigh-performance Kalman filtering algorithm
ApplicationsSatellite tracking; high-voltage transmission tower and pole monitoring; aerial work vehicles; underwater ROV navigation; drilling equipment measurement and control; marine surveying instruments; robot control; unmanned aircraft
SOURCE WITH CHINADRONE

Request a quote for BW-AH55

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 ↗
Flight control & navigation

BW-MINS500

By Wuxi Beiwei Sensing Technology

The Wuxi Beiwei Sensing Technology BW-MINS500 is a compact micro inertial navigation system intended for unmanned aircraft, robotics and other vehicle or stabilization applications. Its 60 × 59 × 29 mm envelope, 9–36V DC supply and selectable serial interfaces support host-platform integration, with specified attitude accuracy, heading retention and temperature-qualified inertial sensor performance.

CUAV X7+ flight controller with silver housing and black connector base.
Flight control & navigation

CUAV X7+ Flight Controller

By CUAV

The CUAV X7+ Flight Controller combines an STM32H743 processor, three IMU sensor sets and a modular carrier-board design for academic research and commercial systems integration. It supports ArduPilot and PX4 firmware, provides 14 PWM outputs with Dshot on 12, and requires separate controller and servo power supplies.

Flight control & navigation

BW-MINS300

By BWSENSING

The 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.