• DocumentCode
    3069020
  • Title

    SEDSAT solar array output power analysis

  • Author

    Wang, Yongqian ; Maier, Mark

  • Author_Institution
    Beijing Inst. of Spacecraft Syst. Eng., China
  • fYear
    1998
  • fDate
    8-10 Mar 1998
  • Firstpage
    345
  • Lastpage
    349
  • Abstract
    This paper analyzes SEDSAT´s solar array´s illumination and power conditions. It uses the method of coordinate frame transformation to compute the sun angles on the solar arrays. It defines the solar array´s normal direction in the geocentric orbital coordinate So, and then gets the new normal direction of solar array at the viewer frame (from the sun). The method can be applied on any kind of orbit. It is a numerical calculation method and easily calculated on a computer. This paper also uses a solar array model to calculate SEDSAT´s I-V and power curves. By combining the illumination with solar array´s model, SEDSAT solar panel´s output power profiles are worked out. These results are very useful for evaluating SEDSAT´s power management strategies
  • Keywords
    artificial satellites; solar cell arrays; space vehicle power plants; I-V curves; SEDSAT solar array output power analysis; coordinate frame transformation; geocentric orbital coordinate; numerical calculation method; output power profiles; power curves; power management; solar array illumination; solar array power conditions; sun angles; Aerospace engineering; Earth; Equations; Power engineering and energy; Power engineering computing; Power generation; Satellites; Space vehicles; Sun; Systems engineering and theory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    System Theory, 1998. Proceedings of the Thirtieth Southeastern Symposium on
  • Conference_Location
    Morgantown, WV
  • ISSN
    0094-2898
  • Print_ISBN
    0-7803-4547-9
  • Type

    conf

  • DOI
    10.1109/SSST.1998.660090
  • Filename
    660090