書誌事項
- タイトル別名
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- Mechanism of Roll Control Response Characteristics in an Aircraft and a Paraglider
- ヒコウキ ト パラグライダ ニ オケル ヨコユレ ソウダ オウトウ トクセイ ノ ソウイ メカニズム
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There are two interesting differences in roll control response characteristics between an aircraft and a paraglider: 1) Opposite roll angle is generated by the same control surface deflection: and 2) to keep the roll angle constant, an aircraft requires a pilot to return the control wheel to the nearly neutral position, but a paraglider requires him to keep the control surface deflection. Although it is commonly accepted that the main factor producing these differences would be the adverse yaw characteristics, the essential mechanism has not yet been clearly determined. This study focuses on features in their airframe configurations, and aims to determine the physical mechanism which produces their differences in roll control responses. Results showed that not only adverse yaw characteristics but also lower center of gravity position and decrease of vertical fin area in a paraglider are the main parameters.
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 55 (642), 337-343, 2007
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
- 1390001204470735232
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- NII論文ID
- 10019783925
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 8893982
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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