• DocumentCode
    1157126
  • Title

    Attitude stabilization with actuators subject to switching restrictions: an approach via exact relay control methods

  • Author

    Kienitz, Karl Heinz

  • Author_Institution
    Instituto Technologico de Aeronaut., Divisao de Engenharia Eletronica, Sao Jose dos Campos
  • Volume
    42
  • Issue
    4
  • fYear
    2006
  • fDate
    10/1/2006 12:00:00 AM
  • Firstpage
    1485
  • Lastpage
    1492
  • Abstract
    On-off thrusters are frequently used as actuators for attitude control. Typically these thrusters are subject to switching constraints. A limit cycle is the normal steady state operation mode of such attitude control systems. This contribution deals with controller design for precision attitude stabilization using actuators whose switching restrictions are explicitly considered. An exact approach is presented using ideas from established relay control methods. The design procedure is illustrated with an attitude controller design to attain a limit cycle with prescribed characteristics
  • Keywords
    actuators; attitude control; relay control; actuators; attitude control systems; precision attitude stabilization; relay control methods; steady state operation; switching restrictions; Actuators; Attitude control; Control systems; Design methodology; Limit-cycles; Propellants; Relays; Space vehicles; State-space methods; Steady-state;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2006.314588
  • Filename
    4107990