• DocumentCode
    391138
  • Title

    Local equilibrium controllability of the triaxial attitude control testbed

  • Author

    Jinglai Shen ; McClamroch, N. Harris ; Bloch, Anthony M.

  • Author_Institution
    Dept. of Aerosp. Eng., Michigan Univ., Ann Arbor, MI, USA
  • Volume
    1
  • fYear
    2002
  • fDate
    10-13 Dec. 2002
  • Firstpage
    528
  • Abstract
    Local configuration controllability and local equilibrium controllability of the Triaxial attitude control testbed (TACT) are studied. The TACT is controlled only by a class of actuators referred to as shape actuators. This implies that there is a conserved quantity and there is a base body equilibrium manifold at each fixed shape. Thus, the TACT states are not small time locally controllable at equilibrium. But a weaker configuration controllability and equilibrium controllability property may be satisfied at an equilibrium. Important symmetric product formulas and properties are obtained. These properties explicitly show dynamic coupling and symmetry of the TACT. Based on these properties, local equilibrium controllability analysis is carried out for the TACT with fully actuated shape variables. Sufficient conditions for local equilibrium controllability are presented for three examples.
  • Keywords
    aerospace test facilities; attitude control; controllability; space vehicles; symmetry; dynamic coupling; local configuration controllability; local equilibrium controllability; shape actuators; sufficient conditions; symmetric product formulas; symmetry; triaxial attitude control testbed; Actuators; Aerodynamics; Aerospace testing; Control systems; Controllability; Mathematics; Mechanical systems; Shape control; Space vehicles; Velocity control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-7516-5
  • Type

    conf

  • DOI
    10.1109/CDC.2002.1184550
  • Filename
    1184550