• DocumentCode
    728208
  • Title

    Synchrophasing control in a multi-propeller driven aircraft

  • Author

    Xianghua Huang ; Yangyang Wang ; Long Sheng

  • Author_Institution
    JiangSu Province Key Lab. of Aerosp. Power Syst., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
  • fYear
    2015
  • fDate
    1-3 July 2015
  • Firstpage
    1836
  • Lastpage
    1841
  • Abstract
    Propeller synchrophasing control is an active noise control technology with high feasibility and significant effect among various kinds of passive and active methods. A simple and effective synchrophasing control strategy was proposed based on the relationship analysis of phase and angular displacement. Digital simulations and experiments of synchrophasing platform which adopts two propellers driven by servo motors verified that the control strategy can reduce the phase vibration because of external disturbance on propellers. Two synchrophasing control methods, including speed command correction and integrated speed/power command correction, are introduced to solve the synchrophasing control on the existing integrated speed/command control system. Simulation results based on a turboprop engine component level model show that the latter has the merits of rapid response swiftness, high precision and effective suppression of limit circle caused by actuator deadband.
  • Keywords
    aerospace propulsion; aircraft control; noise abatement; propellers; servomotors; active noise control technology; actuator deadband; angular displacement; external disturbance; multipropeller driven aircraft; phase displacement; phase vibration reduction; power command correction; propeller synchrophasing control; relationship analysis; servo motors; speed command correction; turboprop engine component level model; Actuators; Engines; Fuels; Noise; Propellers; Velocity control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2015
  • Conference_Location
    Chicago, IL
  • Print_ISBN
    978-1-4799-8685-9
  • Type

    conf

  • DOI
    10.1109/ACC.2015.7171000
  • Filename
    7171000