• DocumentCode
    2593375
  • Title

    Curved path approaches and dynamic interpolation

  • Author

    Jackson, Joseph W. ; Crouch, Peter E.

  • Author_Institution
    Honeywell Inc., Glendale, AZ, USA
  • fYear
    1990
  • fDate
    15-18 Oct 1990
  • Firstpage
    404
  • Lastpage
    408
  • Abstract
    The method of splines was applied to the control of linearizable dynamical systems such that an affine invariant cost functional (total energy) is minimized subject to discrete path constraints. CAGD (computer-aided geometric design) and optimal control methods were applied to derive reference trajectories for comparison with the dynamic results, and to determine intercept times for the waypoints. An acceptable trajectory was generated by the application of these methods to a difficult aircraft approach problem. It is suggested that a combination of finite element and spline techniques should eventually be suitable for solutions of practical dynamic interpolation problems considered in the literature
  • Keywords
    aerospace computing; aircraft control; control system CAD; finite element analysis; interpolation; optimal control; splines (mathematics); affine invariant cost functional; aircraft approach; computer-aided geometric design; curved path approach; discrete path constraints; dynamic interpolation; finite element analysis; intercept times; linearizable dynamical systems; optimal control; reference trajectories; splines; total energy; Aerospace engineering; Air traffic control; Aircraft; Airports; Control systems; Design engineering; Flexible manufacturing systems; Interpolation; Spline; Systems engineering and theory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 1990. Proceedings., IEEE/AIAA/NASA 9th
  • Conference_Location
    Virginia Beach, VA
  • Type

    conf

  • DOI
    10.1109/DASC.1990.111322
  • Filename
    111322