• DocumentCode
    665183
  • Title

    The quaternion-based attitude control system with an augmented dynamic

  • Author

    Septanto, Harry ; Trilaksono, B. Riyanto ; Syaichu-Rohman, Arief ; Poetro, Ridanto Eko ; Ibrahim, A.R.

  • Author_Institution
    Sch. of Electr. Eng. & Inf., Inst. Teknol. Bandung, Bandung, Indonesia
  • fYear
    2013
  • fDate
    7-8 Nov. 2013
  • Firstpage
    190
  • Lastpage
    193
  • Abstract
    Quaternion-based attitude determination system is considered since it can represent all physical attitudes, but not uniquely. An inappropriate quaternion-based control law would imply to a non-efficient control effort and difficulty in guaranteeing global stability. Many research efforts decide to add complexity in the controller by using jump-discontinuity function and/ or hybrid system. In contrast, this paper proposes a continuous quaternion-based attitude control system with an augmented dynamic that guaranteed to be able to regulate any physical state asymptotically. The effectiveness of the designed system is verified through simulations.
  • Keywords
    attitude control; augmented dynamic; continuous quaternion-based attitude control system; hybrid system; jump-discontinuity function; physical attitudes; quaternion-based attitude determination system; quaternion-based control law; Kinematics; Space vehicles; asymptotically stable; augmented dynamic; quaternion; spacecraft attitude control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation, Communications, Information Technology, and Biomedical Engineering (ICICI-BME), 2013 3rd International Conference on
  • Conference_Location
    Bandung
  • Print_ISBN
    978-1-4799-1649-8
  • Type

    conf

  • DOI
    10.1109/ICICI-BME.2013.6698490
  • Filename
    6698490