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A Series Flight Control：
A3A4A5
B Series Flight Control：
B2B4B7B8
E Series Flight Control：
E1
M Series Flight Control：
Ultra-Micro Flight Control
XF Series Flight Control：
XF10XF20
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A4 series flight control and navigation computer: suitable for small, electric, fixed-wing, tiltorotor, quadcopter, and other aircraft.
B7 series flight control and navigation computer: suitable for all quadcopters.
XF20 is a standard autonomous vehicle: supports GNSS guidance and cockpit guidance, suitable for fixed-wing aircraft, multiple task routes.
SESRVICE & SUPPORT
Design and Simulation Service
Software Development Service
Hardware Development Service
Integration Testing Service
Flight Testing Service
Typical Case - Fixed Wing
Typical Case - Vertical Take-off and Landing
Typical Case - Multiple-copter
Typical Case - Special Application
Typical Case - Patrol guidance
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HomeProduct CenterFlight Control and Navigation ComputerXF Series flight control - XF20
XF Series flight control - XF20
The XF20 is a standard autopilot that supports GNSS guidance and pod guidance, and supports various types of fixed wing and various types of mission routes.
Innovation Creation Specialties Focus
Demand driven UAV navigation guidance and control system servicer.
Product Features
  • Suitable for all kinds of fixed wing aircraft, aircraft configuration can be configured.
  • GNSS guidance and pod guidance are adopted.
  • With engine ignition control function.
  • Support ground speed, airspeed flight.
  • With GNSS signal loss protection, timeout without connection can control aircraft self-destruct, function can be disabled.
  • Electronic fence and no-fly zone can be customized, aircraft self-destruct can be controlled, function can be disabled.
  • No flight data recording function to ensure information security.
  • Independent power supply for servo actuator.
  • Support to set a variety of flight routes, set to fly to the target direction, hide the location of the launch point, bypass the dense blockade area.
  • Low voltage, remote control signal loss, radio loss can continue to perform the task, no return event.
  • Configurable launch mode.
  • Configurable power and rudder starting logic.
  • With control parameter binding function.
  • Internal integrated GNSS/IMU navigation.
  • External magnetometer supports calibration of magnetic compass before installation.
  • Navigation has self-alignment function, supports moving base alignment.
    • Survive by quality, develop by reputation, and continue to create value for customers
    Performance Parameters
    System Performance
    Attitude Accuracy RMS
    1°
    Heading Accuracy RMS
    2°
    Single Point Positioning Accuracy
    2.5m
    Single Point Velocity Accuracy
    0.1m/s
    Airspeed Accuracy 1σ
    2m/s
    Airspeed Measurement Range
    ≤0.3Ma
    Altitude Measurement Range
    <18000m
    Servomechanism/Motor Update Frequency
    ≤400Hz
    Servomechanism Power Supply
    Current ≤3A, unlimited voltage
    External Interface
    TTL
    3
    SBUS
    1
    PWM
    8
    CAN
    1
    AD
    2
    IO
    1 (reusable as PWM)
    Electrical Parameter
    Supply Voltage
    DC5±0.5V
    Power Consumption
    ＜1W
    Physical Parameter
    Dimension
    89mm×57mm×28mm
    Weight
    173g
    Environmental Parameter
    Operating Temperature
    -20℃~55℃
    Storage Temperature
    -40℃~85℃
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