• DocumentCode
    382415
  • Title

    Ellipsoid methods for formation flying control of two nano-satellites

  • Author

    Veres, S.M. ; Rokitianski, D.Ya. ; Gabriel, S.B. ; Rogers, E.

  • Author_Institution
    Sch. of Eng. Sci., Southampton Univ., UK
  • Volume
    1
  • fYear
    2002
  • fDate
    2002
  • Firstpage
    298
  • Abstract
    The paper provides analysis and implementable ellipsoid-based solutions to the constrained control problems of stabilization and manoeuvre control of two nano-satellites. The solutions under ellipsoid constraints of actuators and measurements are considered, covering input magnitude constraints, bounded disturbances and measurement errors. An example illustrates the presented method with simulation of the motion of a nano-satellite pair.
  • Keywords
    actuators; aerospace control; artificial satellites; measurement errors; stability; actuators; bounded disturbances; constrained control problems; ellipsoid methods; formation flying control; input magnitude constraints; manoeuvre control; measurement errors; measurements; nano-satellites; stabilization; Actuators; Computer science; Ellipsoids; Equations; Master-slave; Measurement errors; Motion analysis; Robust control; Satellites; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 2002. Proceedings of the 2002 International Conference on
  • Print_ISBN
    0-7803-7386-3
  • Type

    conf

  • DOI
    10.1109/CCA.2002.1040202
  • Filename
    1040202
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=382415