• DocumentCode
    3575727
  • Title

    Sampled-data representation for relative motion along elliptical orbits

  • Author

    Yafei Li ; Genting Yan ; Yuzhi Xiao

  • Author_Institution
    Aerosp. Syst. Eng. Shanghai, Shanghai, China
  • fYear
    2014
  • Firstpage
    381
  • Lastpage
    386
  • Abstract
    This paper concerns with the dynamics of TH equations both in the time domain and in the true anomaly domain. Based on the homogeneous solutions of TH equations, a state transition matrix for the TH equations in the true anomaly domain is obtained. The state transition matrix applies to any eccentric orbit. Through the state transition matrix, the sampleddata descriptions are obtained for both the TH equations and the dimensionless equations. In order to evaluate the sampleddata description presented in this paper, a discrete time model constructed by the state transition matrix derived by Melton is introduced. At last simulations present the errors between these sampled-data descriptions.
  • Keywords
    artificial satellites; discrete time systems; matrix algebra; sampled data systems; TH equations; dimensionless equations; discrete time model; eccentric orbit; elliptical orbits; sampled-data representation; state transition matrix; true anomaly domain; Acceleration; Differential equations; Mathematical model; Orbits; Radio frequency; Satellites; Time-domain analysis;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronics and Control (ICMC), 2014 International Conference on
  • Print_ISBN
    978-1-4799-2537-7
  • Type

    conf

  • DOI
    10.1109/ICMC.2014.7231583
  • Filename
    7231583