The orbit estimation for low thrust spacecraft

説明

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.

収録刊行物

詳細情報 詳細情報について

  • CRID
    1390282680560655488
  • NII論文ID
    130006960013
  • DOI
    10.11499/sicep.2002.0.404.0
  • 本文言語コード
    en
  • データソース種別
    • JaLC
    • CiNii Articles
  • 抄録ライセンスフラグ
    使用不可

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