• DocumentCode
    2370961
  • Title

    Design of a novel type of intelligent DDV actuator system for aeroplane

  • Author

    Tian, Yong ; Li, Tian ; Shao, Shan

  • Author_Institution
    Sch. of Aeronaut. Sci. & Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
  • fYear
    2012
  • fDate
    23-25 March 2012
  • Firstpage
    181
  • Lastpage
    184
  • Abstract
    This paper mainly focuses on the design of a novel type of intelligent DDV actuator system for aeroplane. The function, structure principle and redundancy management of the intelligent DDV (Direct-Drive-Valve) servo actuator system for aeroplane is described in detail. The intelligent DDV servo actuator which is the important part of the system is also described in the paper, including the structure and performance characteristic, the key technique, and so on. An experiment is conducted to verify the dynamic performance and fault monitoring function of the new system. The hardware-in-loop experimental results prove that the design and application of the intelligent DDV servo actuator system on some aeroplane could solve the technical problems in real world. Also, the control precision, stability, and fault monitoring of the system can perfectly satisfy the aeroplane control system design requirements.
  • Keywords
    aircraft control; control system synthesis; drives; fault diagnosis; intelligent actuators; servomechanisms; stability; valves; aeroplane control system design; direct drive valve; fault monitoring function; hardware-in-loop; intelligent DDV servo actuator system; redundancy management; stability; structure principle; Actuators; Artificial intelligence; Circuit faults; Monitoring; Redundancy; Servomotors; Valves;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Information Science and Technology (ICIST), 2012 International Conference on
  • Conference_Location
    Hubei
  • Print_ISBN
    978-1-4577-0343-0
  • Type

    conf

  • DOI
    10.1109/ICIST.2012.6221633
  • Filename
    6221633