書誌事項
- タイトル別名
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- Flight Control Designs of Unmanned Space Vehicle Using Linear Interpolation Gain Scheduling.
- センケイ ホカン ゲインスケジューリング オ モチイタ ムジン ウチュウ オウカンキ ノ ヒコウ セイギョケイ セッケイ
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This paper presents flight control designs of an unmanned space vehicle, HOPE-X, vehicle using interpolation gain scheduling techniques. There are three flight phases from deorbit to landing in HOPE-X; reentry, terminal area energy management (TAEM), and approach and landing. This paper is addressed to the TAEM phase in which an amount of lateral maneuvers are required. Two interpolation gain scheduled state feedback laws were designed with respect to the Lyapunov functions used for guaranteeing the global stability of the closed-loop system, and were applied to the numerical simulations of the HOPE-X. As a result, the gain scheduled control law showed better control performance in the entire of TAEM phase than fixed state feedback laws. The gain scheduling using a parameter-dependent Lyapunov function was superior to the one using a conventional Lyapunov function.
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 50 (582), 278-285, 2002
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
- 1390001204469076992
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- NII論文ID
- 10008967899
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 6222740
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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