• DocumentCode
    700484
  • Title

    Outer flatness: Trajectory generation for a model helicopter

  • Author

    van Nieuwstadt, Michiel ; Murray, Richard M.

  • Author_Institution
    Ford Res. Centre Aachen, Aachen, Germany
  • fYear
    1997
  • fDate
    1-7 July 1997
  • Firstpage
    325
  • Lastpage
    330
  • Abstract
    This paper introduces the concept of outer flatness, a derivative of differential flatness. Outer flatness describes a system that can be split in 2 subsytems, a non-flat inner system and a flat outer system. The outputs of the outer system are the tracking outputs of interest. The inputs of the outer system are the outputs of the inner system, and not subject to our direct control. The inputs of the inner system are the real actuator inputs. This system structure is also present in backstepping and dynamic inversion. We present two theorems on exponential and bounded tracking for outer flat systems, based on Lyapunoff arguments. We validate the approach with simulations and experiments on a model helicopter.
  • Keywords
    aircraft control; control nonlinearities; differential equations; helicopters; trajectory control; backstepping; differential flatness; dynamic inversion; exponential tracking; flat outer system; model helicopter; nonflat inner system; outer flatness; trajectory generation; Actuators; Dynamics; Helicopters; Jacobian matrices; Mathematical model; Rotors; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (ECC), 1997 European
  • Conference_Location
    Brussels
  • Print_ISBN
    978-3-9524269-0-6
  • Type

    conf

  • Filename
    7082114