• DocumentCode
    718656
  • Title

    Dynamics and control of angular acceleration of a re-entry spacecraft with a small asymmetry in the atmosphere in the presence of the secondary resonance effect

  • Author

    Lyubimov, V.V.

  • Author_Institution
    Dept. of Higher Math., SSAU, Samara, Russia
  • fYear
    2015
  • fDate
    21-23 May 2015
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    We consider the problem of controlled reduction of angular acceleration of a re-entry spacecraft with a small mass and aerodynamic asymmetry. An analytical dependence is proposed to control the angular acceleration of the spacecraft, providing a reduction in the aerodynamic asymmetry.
  • Keywords
    acceleration control; aerodynamics; resonance; space vehicles; aerodynamic asymmetry; analytical dependence; angular acceleration control; atmosphere asymmetry; controlled reduction problem; mass asymmetry; re-entry spacecraft; secondary resonance effect; Acceleration; Aerodynamics; Angular velocity; Atmospheric modeling; Mathematical model; Space vehicles; angular velocity; asymmetry; control; resonance effect; spacecraft;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Communications (SIBCON), 2015 International Siberian Conference on
  • Conference_Location
    Omsk
  • Print_ISBN
    978-1-4799-7102-2
  • Type

    conf

  • DOI
    10.1109/SIBCON.2015.7147134
  • Filename
    7147134
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=718656