• DocumentCode
    2728017
  • Title

    Consensus-based controllers for spacecraft attitude alignment: Simulation results

  • Author

    Septanto, Harry ; Riyanto-Trilaksono, Bambang ; Syaichu-Rohman, Arief ; Eko-Poetro, Ridanto

  • Author_Institution
    Scool of Electr. Eng. & Inf., Inst. Teknol. Bandung, Bandung, Indonesia
  • fYear
    2011
  • fDate
    8-9 Nov. 2011
  • Firstpage
    52
  • Lastpage
    57
  • Abstract
    Spacecraft formation flying control using consensus algorithm means each spacecraft or satellite in a team updates its state based on the information states of its local neighbours in such a way that the final information state of each agent converges to a common value. This paper discusses spacecraft formation within scope of rotational motions i.e. attitude alignment. Two attitude alignment controllers based on consensus algorithm proposed here.Simulations that run as preliminary proof a concept are presented. Simulations run indicate the proposed control laws might solve the attitude alignment problem i.e. consensus is achieved.
  • Keywords
    attitude control; motion control; space vehicles; attitude alignment; consensus based controllers; control laws; rotational motions; satellite; spacecraft attitude alignment; spacecraft formation flying control; Angular velocity; Attitude control; Biomedical engineering; Instruments; Mathematical model; Space vehicles; Topology; Spacecraft formation flying; attitude alignment; consensus algorithm; nonlinear control system; simulation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation, Communications, Information Technology, and Biomedical Engineering (ICICI-BME), 2011 2nd International Conference on
  • Conference_Location
    Bandung
  • Print_ISBN
    978-1-4577-1167-1
  • Type

    conf

  • DOI
    10.1109/ICICI-BME.2011.6108593
  • Filename
    6108593