• DocumentCode
    718792
  • Title

    Rotational motion of a nanosatellite using onboard electromagnetic coils after collision with a solid high-speed particle

  • Author

    Lyubimov, V.V. ; Osipov, A.A. ; Semkin, N.D.

  • Author_Institution
    Dept. of Higher Math., SSAU, Samara, Russia
  • fYear
    2015
  • fDate
    21-23 May 2015
  • Firstpage
    1
  • Lastpage
    3
  • Abstract
    In this study, we model a collision of a nanosatellite with space debris or micrometeoroids, leading to rotational motion of a nanosatellite. We consider the problem of controlled reduction of acquired angular velocity of a nanosatellite. The control process is based on the use of three electromagnets.
  • Keywords
    artificial satellites; coils; meteoroids; space debris; angular velocity; control process; micrometeoroids; nanosatellite; onboard electromagnetic coils; rotational motion; solid high-speed particle collision; space debris; Angular velocity; Coils; Damping; Magnetomechanical effects; Mathematical model; Satellites; Space debris; coil; control; nanosatellite; rotation; space debris;
  • 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.2015.7147298
  • Filename
    7147298
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=718792