The orbit estimation for low thrust spacecraft
-
- Ichikawa Tsutomu
- Institute of Space and Astronautical Science (ISAS)
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
-
- SICE Annual Conference Program and Abstracts
-
SICE Annual Conference Program and Abstracts 2002 (0), 404-404, 2002
公益社団法人 計測自動制御学会
- Tweet
詳細情報 詳細情報について
-
- CRID
- 1390282680560655488
-
- NII論文ID
- 130006960013
-
- 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