• DocumentCode
    3083895
  • Title

    Time optimal slewing of flexible spacecraft

  • Author

    Ben-Asher, Joseph ; Burns, J.A. ; Cliff, E.M.

  • Author_Institution
    Virginia Polytechnic Institute and State University, Blacksburg, Virginia
  • Volume
    26
  • fYear
    1987
  • fDate
    9-11 Dec. 1987
  • Firstpage
    524
  • Lastpage
    528
  • Abstract
    The tune optimal slewing problem of flexible spacecraft is considered. The system is discretized by the assumed modes method, and the problem is solved for a linearized model in reduced state space by parameter optimization. Optimality is verified by the maximal principle. The linear solution is further used to obtain time optimal solutions for the non-linear problem.
  • Keywords
    Boundary conditions; Control systems; Cost function; Differential equations; Fuels; Optimal control; Parametric study; Space vehicles; State-space methods; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1987. 26th IEEE Conference on
  • Conference_Location
    Los Angeles, California, USA
  • Type

    conf

  • DOI
    10.1109/CDC.1987.272896
  • Filename
    4049322
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3083895