• DocumentCode
    1601536
  • Title

    Control of gimbal dynamics via sensitivity models for uncertainty in friction parameters

  • Author

    Schoenwald, D. ; Özgüner, Ü ; Graham, R.

  • Author_Institution
    Dept. of Electr. Eng., Ohio State Univ., Columbus, OH, USA
  • fYear
    1992
  • Firstpage
    52
  • Abstract
    Tracking control of the beta gimbals for the solar array panels on the space station Freedom is investigated. In particular, the issue of control in the presence of uncertainty in motor friction parameters is addressed. The impact of parametric uncertainty on gimbal performance is analyzed by incorporating sensitivity functions in the feedback loop to desensitize the gimbal control law to parameter variations. The simulation results indicate that the inclusion of one particular sensitivity function yields some improvements in closed-loop performance when friction parameters are varied from their nominal values
  • Keywords
    aerospace control; attitude control; feedback; sensitivity; solar cell arrays; space vehicle power plants; tracking systems; beta gimbals; closed-loop performance; feedback loop; friction parameter uncertainty; gimbal dynamics control; motor friction parameters; parametric uncertainty; sensitivity models; solar array panels; space station Freedom; tracking control; Actuators; Angular velocity; Feedback loop; Friction; Motor drives; NASA; Optimal control; Performance analysis; Space stations; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 1992., First IEEE Conference on
  • Conference_Location
    Dayton, OH
  • Print_ISBN
    0-7803-0047-5
  • Type

    conf

  • DOI
    10.1109/CCA.1992.269899
  • Filename
    269899