• DocumentCode
    1537764
  • Title

    Naive control of the double integrator

  • Author

    Rao, Venkatesh G. ; Bernstein, Dennis S.

  • Author_Institution
    Dept. of Aerosp. Eng., Michigan Univ., Ann Arbor, MI, USA
  • Volume
    21
  • Issue
    5
  • fYear
    2001
  • fDate
    10/1/2001 12:00:00 AM
  • Firstpage
    86
  • Lastpage
    97
  • Abstract
    We deal with a form of controller evaluation that may be called naive control. In naive control, a control algorithm derived under nominal (or ideal) conditions is evaluated by analytical or numerical means under off-nominal (or nonideal) conditions that were not assumed in the formal synthesis procedure. Under such nonideal conditions, the controller may or may not perform well. This approach is distinct from robust control, which seeks to accommodate off-nominal perturbations in the synthesis procedure. We consider the double integrator plant, which is one of the most fundamental systems in control applications, representing single degree-of-freedom translational and rotational motion. Applications of the double integrator include low-friction, free rigid-body motion, such as single-axis spacecraft rotation and rotary crane motion. The double integrator plant considered includes a saturation nonlinearity on the control input
  • Keywords
    control nonlinearities; control system synthesis; cranes; nonlinear control systems; optimal control; space vehicles; stability; control nonlinearity; control synthesis; double integrator; naive control; nonideal conditions; nonlinear control systems; rotary crane; spacecraft; Adaptive control; Control system synthesis; Control systems; Cranes; Motion control; Programmable control; Sliding mode control; Space vehicles; Testing; Velocity control;
  • fLanguage
    English
  • Journal_Title
    Control Systems, IEEE
  • Publisher
    ieee
  • ISSN
    1066-033X
  • Type

    jour

  • DOI
    10.1109/37.954521
  • Filename
    954521