• DocumentCode
    681111
  • Title

    Fault-tolerant actuator control system for a spaceplane using adaptive control

  • Author

    Shimada, Yuzo ; Nakao, Yasuyuki ; Abe, Akio

  • Author_Institution
    Department of Aerospace Engineering, Nihon University, Tokyo, Japan
  • fYear
    2013
  • fDate
    14-17 Sept. 2013
  • Firstpage
    1497
  • Lastpage
    1502
  • Abstract
    In this paper, we present a fault-tolerant actuator control system with redundancy for a future spaceplane. The control system based on model reference adaptive control is designed to maintain the control effects with respect to the vehicle rotational motion, even if some of the actuators develop problems or break down. A hardware-in-the-loop simulation involving real DC servo motors was carried out to show the effectiveness of the proposed system.
  • Keywords
    Actuators; Aerospace control; Equations; Fault tolerance; Fault tolerant systems; Mathematical model; Vectors; ALFLEX; Actuator; Adaptive control; DC motor; Fault-tolerant control; Flight control; Spaceplane;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    SICE Annual Conference (SICE), 2013 Proceedings of
  • Conference_Location
    Nagoya, Japan
  • Type

    conf

  • Filename
    6736279
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=681111