書誌事項
- タイトル別名
-
- Self-Tuning Fuzzy Controlled Mechanical Impulse Method for Angular Momentum Reduction of Malfunctioning Satellite
- キノウ フゼン エイセイ ノ カク ウンドウリョウ ゲンスイ ノ タメ ノ ジリツ ガクシュウガタ ショウゲキ スラストホウ
この論文をさがす
抄録
To repair a malfunctioning satellite or de-orbit a space debris object, capturing free-flying, non-cooperative objects in orbit is required. These objects could be in complicated attitude motions, such as spin, nutation and tumbling, which are obstacles to capturing a non-cooperative object. This paper discusses a fuzzy control applied to reduction of tumbling motion of the non-cooperative object by the repetitive impulses produced by projecting small particles to the non-cooperative object. The purpose of this study is to tune the parameters of the fuzzy controller which determines the direction and velocity of the projection by means of learning algorithm. It is shown that the proposed method has advantage in robustness to variation of motion and geometry of the target.
収録刊行物
-
- 日本航空宇宙学会論文集
-
日本航空宇宙学会論文集 55 (636), 27-33, 2007
一般社団法人 日本航空宇宙学会
- Tweet
詳細情報 詳細情報について
-
- CRID
- 1390282679446692352
-
- NII論文ID
- 130000147080
-
- NII書誌ID
- AA11307372
-
- ISSN
- 24323691
- 13446460
-
- NDL書誌ID
- 8654081
-
- 本文言語コード
- ja
-
- データソース種別
-
- JaLC
- NDL
- Crossref
- CiNii Articles
-
- 抄録ライセンスフラグ
- 使用不可