書誌事項
- タイトル別名
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- Orbital Transfer of a Tethered Satellite System Using Pitching Motion Control through Tether Length Variation
- テザーチョウ ヘンカ ニ ヨル ピッチング ウンドウ セイギョ オ リヨウシタ テザー エイセイ ノ キドウ ヘンカン
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This study deals with orbital transfer of a tethered satellite system in equatorial plane through its tether length control. Since tether length variation generates diversely different pitching motion on an elliptic orbit, appropriately designed tether length profiles can give the satellites a desired velocity-vector-increment at a prescribed position in orbit. This paper proposes a procedure to get an adequate control input profile which attains the designated states at the final position by applying nonlinear control method. Also the procedure can directly cope with physical restrictions for the system, such as the maximum tether length or tether tension. The proposed procedure consists of three steps associated with control for its angular momentum of pitching motion, which finally leads to control of tether length, pitch angular rate, and pitch angle at the final position, respectively.
収録刊行物
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- 日本航空宇宙学会論文集
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日本航空宇宙学会論文集 56 (654), 308-314, 2008
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390001204468699904
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- NII論文ID
- 10024595602
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 9585466
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可