• DocumentCode
    2944603
  • Title

    Real-time guidance of reusable winged space plane using genetic algorithm implemented on field programmable gate array

  • Author

    Miyamoto, S. ; Narumi, T. ; Matsumoto, T. ; Yonemoto, K.

  • Author_Institution
    Kyushu Inst. of Technol., Fukuoka, Japan
  • fYear
    2012
  • fDate
    11-14 July 2012
  • Firstpage
    349
  • Lastpage
    354
  • Abstract
    An efficient and flexible real-time guidance system is one of the critical needs in the development of a future reusable space transportation system. The genetic algorithm employs an optimization model called the evolution of life, which is generally considered numerically robust but involves an extremely high calculation cost. To reduce the cost, this paper proposes an efficient procedure that optimizes the coefficients of a set of prescribed input functions. In addition, to reduce the calculation time by more than one tenth, the optimization scheme is implemented on a field programmable gate array. The resultant optimization system is applied to an on-board guidance system that optimizes the trajectory of an experimental winged rocket in real time.
  • Keywords
    aerospace components; field programmable gate arrays; genetic algorithms; rockets; space vehicles; field programmable gate array; genetic algorithm; on-board guidance system; optimization model; real-time guidance; resultant optimization system; reusable space transportation system; reusable winged space plane; Computer aided software engineering; Erbium; Field programmable gate arrays; Genetic algorithms; Optimization; Rockets; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Advanced Intelligent Mechatronics (AIM), 2012 IEEE/ASME International Conference on
  • Conference_Location
    Kachsiung
  • ISSN
    2159-6247
  • Print_ISBN
    978-1-4673-2575-2
  • Type

    conf

  • DOI
    10.1109/AIM.2012.6266008
  • Filename
    6266008