• DocumentCode
    2434835
  • Title

    Embedding FDI in launcher attitude controllers

  • Author

    Ramos, Fausto ; Alazard, Daniel

  • Author_Institution
    ISAE, Univ. de Toulouse, Toulouse, France
  • fYear
    2009
  • fDate
    11-13 June 2009
  • Firstpage
    609
  • Lastpage
    614
  • Abstract
    It looks interesting the idea of obtaining more than a controller after designing a control system. In fact, given some conditions, it is possible to rearrange the controller states, revealing an observer structure, without changing the original system. Such proposition does not only means that the estimations of the plant states are available, but also that fault estimators can be built, providing an unexpected horizon of fault tolerance and even control reconfiguration. In order to illustrate that, a generalization aimed at obtaining observer-based forms from augmented, reduced or full order controllers will be applied to a launcher model, subject to sensor faults and external disturbance.
  • Keywords
    attitude control; control system synthesis; fault diagnosis; fault tolerance; observers; state estimation; FDI; control system design; even control reconfiguration; fault detection-and-isolation; fault tolerance; launcher attitude controller; observer structure; plant state estimation; Aerospace control; Attitude control; Control systems; Fault detection; Fault tolerance; Nonlinear control systems; Observers; Robust control; Robust stability; State estimation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Recent Advances in Space Technologies, 2009. RAST '09. 4th International Conference on
  • Conference_Location
    Istanbul
  • Print_ISBN
    978-1-4244-3627-9
  • Electronic_ISBN
    978-1-4244-3628-6
  • Type

    conf

  • DOI
    10.1109/RAST.2009.5158264
  • Filename
    5158264