• DocumentCode
    2300860
  • Title

    Aircraft route optimization using adaptive simulated annealing

  • Author

    Kastella, Keith

  • Author_Institution
    Unisys Electron. & Inf. Syst. Group, Eagan, MN, USA
  • fYear
    1991
  • fDate
    20-24 May 1991
  • Firstpage
    1123
  • Abstract
    It is demonstrated that simulated annealing (SA) is a viable optimization method for use in route optimization for aircraft flying in tactical attack roles at low altitude deep in enemy territory. It is found that adaptive control of the temperature based on a heuristic measure of equilibrium greatly reduces the algorithm´s sensitivity to the cooling rate while giving a 5- to 10-fold speed-up with no adverse impact on the quality of the solutions produced. These results scale nearly linearly with problem size
  • Keywords
    adaptive control; aircraft; military systems; optimisation; scheduling; simulated annealing; adaptive control; adaptive simulated annealing; aircraft; analogy; cooling rate; equilibrium; heuristic measure; route optimization; tactical attack; Aerospace electronics; Aircraft; Cooling; Information systems; Leg; Meeting planning; Optimization methods; Simulated annealing; Stochastic processes; Temperature sensors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace and Electronics Conference, 1991. NAECON 1991., Proceedings of the IEEE 1991 National
  • Conference_Location
    Dayton, OH
  • Print_ISBN
    0-7803-0085-8
  • Type

    conf

  • DOI
    10.1109/NAECON.1991.165900
  • Filename
    165900