ADCOM-3D FCU FLIGHT CONTROL UNIT

     

    Overview

     

     
      ADCOM-3D FCU is a flight control unit designed with latest electronic technology using advanced digital processing techniques for control and measurements.
    This FCU can be used as independent inertial and GPS navigation unit in targets and UAVs.

     

    Features
      • Attitude and heading reference correction, using strap down Inertial Measurement Unit (IMU) with GPS and 3-axes magnetometer feedback
    • Onboard flight data recording
    • Air vehicle stabilization and control by user-defined profiles
    • Auto Navigation
    • Change of flight profile from ground control station at any stage of the flight
    • Automatic take-off (Auto launch)
    • Automatic landing approach by GPS and laser altimeter (optional)
    • Auto Recovery Function
    • Fail-safe function (if uplink is interrupted)
    • Fault identification and automatic guidance to a preset landing point at emergency cases
    • Control of various types of payloads

     

    Specifications
     

    • Max. angular speed: ± 150 deg/s
    • Max. acceleration: ± 2 g
    • Measurement of static and dynamic pressure
    • Independent angle measurement on 3-axes
    • Thermal compensation of sensors
    • eCAN bus configuration for interfacing servos, transceiver unit, laser altimeter and other peripherals
    • 3-axes magnetometer interface
    • Capability to control up to 16 payloads
    • 2 serial (RS 232) ports available
    • Power supply 9–18 V @ 300 mA, with over voltage and polarity protection
    • Dimensions: 200 x 110 x 50 (mm) (without mounting fittings)
    • Weight: 0.9 kg
    • Operation temp: -20 to +70o C.