• DocumentCode
    1900332
  • Title

    Aggressive flight maneuvers

  • Author

    Hauser, John ; Hindman, Rick

  • Author_Institution
    Dept. of Electr. & Comput. Eng., Colorado Univ., Boulder, CO, USA
  • Volume
    5
  • fYear
    1997
  • fDate
    10-12 Dec 1997
  • Firstpage
    4186
  • Abstract
    We present a strategy for obtaining aggressive flight maneuvers similar to what might be produced by a pilot. We use a highly simplified aircraft model that can account for the lift/drag and thrust characteristics of an aircraft under consideration. When thrust is considered an input, this model is differentially flat (and dynamically feedback linearizable) so that the system can be made to follow any reasonable trajectory. Most trajectories will require significant movement of the throttle. Except in close formation, a pilot does not tend to make rapid throttle adjustments. Indeed, many maneuvers are accomplished using a fixed throttle position. The objective is to fly a desired path rather than a (time indexed) trajectory. Although the aircraft model with throttle fixed (thrust predetermined) is no longer differentially flat, we show that the system can still be made to follow any reasonable path. Roughly speaking, an appropriate derivative of the path parametrization variable acts as the missing control allowing flatness-like results to be obtained
  • Keywords
    aircraft control; attitude control; differential equations; feedback; matrix algebra; aggressive flight maneuvers; differentially flat model; dynamically feedback linearizable model; fixed throttle position; lift/drag characteristics; simplified aircraft model; thrust characteristics; trajectory following; Acceleration; Aerospace control; Aerospace engineering; Aerospace simulation; Military aircraft; Path planning; Stability; Symmetric matrices; Tail; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1997., Proceedings of the 36th IEEE Conference on
  • Conference_Location
    San Diego, CA
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-4187-2
  • Type

    conf

  • DOI
    10.1109/CDC.1997.649490
  • Filename
    649490