• DocumentCode
    286662
  • Title

    Interpolating sliding mode control: an approach to high precision platform control with uncertain dynamics

  • Author

    Dodds, Stephen J.

  • Author_Institution
    Dept. of Electr. & Electron. Eng., East London Univ., Dagenham, UK
  • fYear
    1993
  • fDate
    34134
  • Firstpage
    42461
  • Lastpage
    410
  • Abstract
    The robustness properties of sliding mode control are exploited in achieving high precision manoeuvring of a space platform to which are attached flexible appendages exhibiting an arbitrary number of flexure modes. Continuous control actuators are assumed. The dynamics parameters are assumed to be unknown but to lie within reasonable practical limits. A new continuous form of discrete-time sliding mode control law is employed. The effects of increasing the iteration interval of the onboard algorithm and errors in the assumed forward path DC gain on the precision with which the platform follows a controlled rate slew demand are investigated. The degree of active flexure mode damping is also investigated
  • Keywords
    aerospace control; attitude control; discrete time systems; space vehicles; stability; variable structure systems; active flexure mode damping; aerospace control; attitude control; controlled rate slew demand; discrete time systems; flexible appendages; forward path DC gain; robust control; robustness; sliding mode control; space platform; stability; uncertain dynamics; variable structure systems;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    High Accuracy Platform Control in Space, IEE Colloquium on
  • Conference_Location
    London
  • Type

    conf

  • Filename
    255868