• DocumentCode
    1619232
  • Title

    Dual-rate global digital redesign for flight control

  • Author

    Rabbath, C.A. ; Hori, N.

  • Author_Institution
    Defence Res. & Dev. Canada, Canada
  • Volume
    1
  • fYear
    2004
  • Firstpage
    338
  • Abstract
    This paper proposes a dual-rate global digital redesign method for the design of flight control systems. Given a two-loop continuous-time autopilot, dual-rate digital redesign based on the concept of plant-input-mapping is applied at each operating point. The proposed approach allows to constrain the orders of the discrete-time controllers, which is a significant consideration when gain scheduling of the linear control laws is performed over the flight envelope. The dual-rate digital redesign technique provides satisfactory closed-loop performances over an extended range of sampling rates, as compared with other widely used methods of digital redesign. Numerical simulations of a symmetrical, tail-controlled missile demonstrate the effectiveness of the proposed method.
  • Keywords
    aerospace control; closed loop systems; continuous time systems; discrete time systems; linear systems; closed-loop performance; discrete-time controllers; dual-rate global digital redesign; flight control system; linear control laws; tail-controlled missile;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    SICE 2004 Annual Conference
  • Conference_Location
    Sapporo
  • Print_ISBN
    4-907764-22-7
  • Type

    conf

  • Filename
    1491422