• DocumentCode
    1339627
  • Title

    Near-Optimal Terrain Collision Avoidance Trajectories using Elevation Maps

  • Author

    Malaek, S.M. ; Abbasi, A.

  • Author_Institution
    Dept. of Aerosp. Eng., Sharif Univ. of Technol., Tehran, Iran
  • Volume
    47
  • Issue
    4
  • fYear
    2011
  • fDate
    10/1/2011 12:00:00 AM
  • Firstpage
    2490
  • Lastpage
    2501
  • Abstract
    The main attempt of this paper is to present a new methodology to model a generic low-level flight close to terrain, which guarantees terrain collision avoidance. Benefiting the advantages of high-speed computer technology, this method uses satellite elevation maps to generate so-called "quad-tree forms." The latter is then used to find the optimal trajectories for low-level flights. The novelty of this approach, entitled the "cost map," lies in the integration of aircraft dynamics into the segmented map. This procedure results in some near-optimal trajectories with respect to aircraft dynamics that could easily be used for minimization of flight path together with pilot effort. Different simulations show the method is applicable wherever there is no need for sharp changes in flight level. Nevertheless, the current method could be expanded to three-dimensional terrain avoidance/terrain following flights.
  • Keywords
    aircraft control; collision avoidance; control engineering computing; optimal control; position control; aircraft dynamics integration; generic low level flight; high speed computer technology; map elevation; near optimal terrain collision avoidance trajectory; near optimal trajectories; quad tree form; satellite elevation maps; terrain collision avoidance; Aerospace control; Collision avoidance; Cost function; Heuristic algorithms; Terrain mapping; Trajectory;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2011.6034646
  • Filename
    6034646