• DocumentCode
    329725
  • Title

    Tools and methods for spacecraft control systems: a geno-fuzzy approach

  • Author

    Ortega, Guiilermo ; Girón-Sierra, José M.

  • Author_Institution
    Eur. Space Agency, Noordwijk, Netherlands
  • Volume
    4
  • fYear
    1998
  • fDate
    11-14 Oct 1998
  • Firstpage
    3167
  • Abstract
    The goal of the paper is to analyze which computational methods and modeling tools based on fuzzy logic helped by genetic algorithms are available right now. The emphasis is put on the analyses and design of spacecraft control systems due to their complexity. A spacecraft control system measures the position and attitude of the craft and produces guidance and rotation commands to place it in a specific orbit and with a specific orientation. Spacecraft control units are complex systems difficult to handle during the analysis and design phases of the engineering life cycle. The article describes who-is-who in the development arena of the support tools and methods, which commercial products are available, and which of them are freely obtainable. The state of the art is presented, and the advantages and disadvantages of each system are carefully examined from a critical point of view
  • Keywords
    aerospace control; attitude measurement; control system analysis; control system synthesis; fuzzy control; fuzzy logic; genetic algorithms; position measurement; space vehicles; commercial products; computational methods; engineering life cycle; geno-fuzzy approach; guidance; modeling tools; rotation; spacecraft control systems; support tools; Algorithm design and analysis; Attitude control; Computational modeling; Control systems; Extraterrestrial measurements; Fuzzy logic; Genetic algorithms; Position measurement; Rotation measurement; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems, Man, and Cybernetics, 1998. 1998 IEEE International Conference on
  • Conference_Location
    San Diego, CA
  • ISSN
    1062-922X
  • Print_ISBN
    0-7803-4778-1
  • Type

    conf

  • DOI
    10.1109/ICSMC.1998.726489
  • Filename
    726489