• DocumentCode
    425572
  • Title

    A stochastically optimal feedforward and feedback technique for flight control systems of high performance aircrafts

  • Author

    Campa, Giampiero ; Fravolini, Mario Luca ; Napolitano, Marcello R. ; Perhinschi, Mario G. ; Battipede, Manuela

  • Author_Institution
    Dept. of Mech. & Aerosp. Eng., West Virginia Univ., Morgantown, WV, USA
  • Volume
    2
  • fYear
    2004
  • fDate
    June 30 2004-July 2 2004
  • Firstpage
    1713
  • Abstract
    This paper focuses on a detailed description of a control technique, which has been successfully used in several advanced flight control systems research projects over the past decade. The technique, called stochastically optimal feedforward and feedback technique (SOFFT), directly descends from optimal control, and in particular from explicit model following control (EMFC). Unlike the most used model following techniques, in SOFFT the feedforward and feedback control laws are designed independently of one another. Moreover, this technique relies on different levels of plant models, specifically, a simple plant model is used for the synthesis of the feedback control law, and another plant model, together with a "command" model, are used in the synthesis of the feedforward control laws. It is important to notice that the controller in its final form is nonlinear in nature. This is because the matrices that compose the plant and command models are constantly updated as the aircraft moves throughout the flight envelope, and at least two algebraic Riccati equations (ARE) are solved in real time to compute the feedback and feedforward gains.
  • Keywords
    Riccati equations; aircraft control; control system synthesis; digital simulation; feedback; feedforward; matrix algebra; nonlinear control systems; optimal control; stochastic systems; algebraic Riccati equations; command models; digital simulation; explicit model following control; feedback control law design; feedback control synthesis; feedback gain; feedforward control law design; feedforward control synthesis; feedforward gains; flight control systems; flight envelope; high performance aircrafts; matrix algebra; nonlinear controller; optimal control; plant models; stochastically optimal feedback technique; stochastically optimal feedforward technique;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 2004. Proceedings of the 2004
  • Conference_Location
    Boston, MA, USA
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-8335-4
  • Type

    conf

  • Filename
    1386826