The orbit estimation for low thrust spacecraft

DOI

Description

There are interplanetary mission by using continuously Low-thrust system. This paper is described Earth-based orbit estimation capability for the electric propulsion spacecraft in the light of recent developments both in a few station tracking concepts and in the thrust subsystem error modeling. Both suboptimal and optimal orbit determination performance are determined for a wide range of process noise parameter values.

Journal

Keywords

Details 詳細情報について

  • CRID
    1390282680560655488
  • NII Article ID
    130006960013
  • DOI
    10.11499/sicep.2002.0.404.0
  • Text Lang
    en
  • Data Source
    • JaLC
    • CiNii Articles
  • Abstract License Flag
    Disallowed

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