• DocumentCode
    645927
  • Title

    A new approach to the solution of free rigid body motion for attitude maneuvers

  • Author

    Pagnozzi, Daniele ; Maclean, Craig ; Biggs, James D.

  • Author_Institution
    Dept. of Mech. & Aerosp. Eng., Adv. Space Concepts Lab., Univ. of Strathclyde, Glasgow, UK
  • fYear
    2013
  • fDate
    17-19 July 2013
  • Firstpage
    664
  • Lastpage
    669
  • Abstract
    A Hamiltonian formulation of free rigid body motion defined on the Special Unitary Group SU(2) is used to integrate the system to obtain a convenient quaternion representation for attitude engineering applications. Novel content of this paper concerns applying a modern approach, based on geometric control theory to obtain the kinematic solution in an elegant and compact form. Moreover, this integration leads to an attitude representation which is not Euler-angle-like, thus enhancing its applicability (e.g. to attitude motion design).
  • Keywords
    attitude control; motion control; space vehicles; Hamiltonian formulation; Special Unitary Group; attitude engineering applications; attitude maneuvers; attitude motion design; attitude quaternion representation; free rigid body motion; geometric control theory; kinematic solution; Angular velocity; Attitude control; Equations; Jacobian matrices; Quaternions; Space vehicles; Tracking;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (ECC), 2013 European
  • Conference_Location
    Zurich
  • Type

    conf

  • Filename
    6669123