• DocumentCode
    2675187
  • Title

    Exact dynamic of satellite relative motion under arbitrary zonal harmonic perturbations

  • Author

    Xu, Guangyan ; Xiang, Feng ; Chen, Ying

  • Author_Institution
    Sch. of Autom., Shenyang Aerosp. Univ., Shenyang, China
  • fYear
    2012
  • fDate
    23-25 May 2012
  • Firstpage
    3676
  • Lastpage
    3681
  • Abstract
    To expand the exact dynamic model of satellite relative motion under J2 perturbation, a new model is established which is exactly up to arbitrary zonal harmonic perturbations. Moreover, a set of differential equations in terms of Reference Satellite Variables (RSV) are obtained to describe the satellite motion around the Earth accurately under arbitrary zonal harmonic perturbations. Since no simplification is applied during the derivation, the result is valid for arbitrary eccentric orbits.
  • Keywords
    artificial satellites; differential equations; motion control; perturbation techniques; J2 perturbation; differential equations; eccentric orbits; exact dynamic model; reference satellite variables; satellite motion; satellite relative motion; zonal harmonic perturbations; Dynamics; Earth; Gravity; Harmonic analysis; Mathematical model; Orbits; Satellites; Satellite formation flying; Satellite relative motion; Zonal harmonic perturbations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Decision Conference (CCDC), 2012 24th Chinese
  • Conference_Location
    Taiyuan
  • Print_ISBN
    978-1-4577-2073-4
  • Type

    conf

  • DOI
    10.1109/CCDC.2012.6244588
  • Filename
    6244588
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2675187