B Series flight control - B8
B8 is specifically designed for multi-rotor aircraft operating under high-vibration and heavy-load conditions. It features three sets of industrial-grade MEMS IMUs and an integrated shock absorption design. Coupled with a magnetometer and barometer architecture, it incorporates multi-source fusion algorithms to achieve centimeter-level positioning, emergency protection in all fault scenarios, fully autonomous operation with thousands of waypoints on a single flight path, and long-duration on-board data closed-loop storage. It is the safe and optimal choice for small and medium-sized multi-rotor aircraft operating in high-vibration environments.
Innovation Creation Specialties Focus
Demand driven UAV navigation guidance and control system servicer.
Product Features
  • Suitable for all types of multi-rotor aircraft.
  • Support 10 routes, 1000 waypoints per route.
  • Support external differential GNSS with high-precision positioning and dual antenna heading resolution.
  • Built-in data logger, support more than 10h data storage, support cyclic storage.
  • Support external integrated GNSS/magnetic compass for easy installation in areas with low magnetic interference.
  • Ground station software supports online map, automatic route planning for non-regular areas, patrol line planning, pre-flight check warning and in-flight warning.
  • Complete emergency protection mechanism, including low voltage, GNSS signal loss, remote control failure protection, etc. Electronic fence and emergency landing point can be set.
  • Support RTK real-time kinematic differential positioning for centimeter-level accuracy.
  • Fully autonomous flight control and photo control functions.
  • Support voltage monitoring with built-in low battery protection strategy.
  • Support RTK real-time kinematic differential positioning for centimeter-level accuracy.
  • Multi-sensor data fusion algorithm based on Kalman filter/complementary filter for precise position and attitude estimation.
  • Support multiple manual control and autonomous flight modes.
  • Survive by quality, develop by reputation, and continue to create value for customers
    Performance Parameters
    System Performance
    Attitude Accuracy RMS
    Heading Accuracy RMS
    Dual Antenna Orientation Accuracy RMS
    0.1°(1m baseline)
    Single Point Positioning Accuracy
    2.5m
    Single Point Velocity Accuracy
    0.1m/s
    RTK Positioning Accuracy
    .8cm+1ppm(horizontal) .5cm+1ppm(altitude)
    Altitude Measurement Range
    <18000m
    Number of Routes
    10 (1000 waypoints for each)
    Data Logging
    10h cyclic storage
    Servo/Motor Update Frequency
    ≤500Hz
    External Interface
    TTL
    5
    CAN
    4
    SBUS
    1 (input), 1 (output)
    PWM
    16
    AD
    2 (input range 0~20V)
    Electrical Parameter
    Supply Voltage
    DC5~5.5V
    Power Consumption
    <1.5W
    Physical Parameter
    Dimension
    76mmx73mmx29mm
    Weight
    138g
    Environmental Parameter
    Operating Temperature
    -20℃~60℃
    Storage Temperature
    -40℃~70℃