書誌事項
- タイトル別名
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- High Performance Prop-hanging Flight Control of Fixed-wing Aircraft Using Quaternions
- クオータニオン オ モチイタ コガタ コテイヨクキ ノ コウセイノウ Prop-Hanging ヒコウ セイギョ
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This paper presents the result of the high performance prop-hanging flight control using quaternions. Prop-hanging flight is known as a way of flight for the fixed-wing aircraft, and it can achieve hovering without special equipments to change the direction of the thrust. We had already succeeded in stabilizing the aircraft during prop-hanging flight using LQI controllers based on the mathematical model. However, a high degree of freedom flight control could not be performed because Euler angles which may cause gimbal lock were used to represent the attitude of the aircraft. In this paper, we utilize quaternions to achieve a high degree of freedom flight control during prop-hanging flight. The effectiveness of the proposed method is evaluated by experiments.
収録刊行物
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- 計測自動制御学会論文集
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計測自動制御学会論文集 49 (2), 275-283, 2013
公益社団法人 計測自動制御学会
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詳細情報 詳細情報について
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- CRID
- 1390282679481130368
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- NII論文ID
- 10031154996
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- NII書誌ID
- AN00072392
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- ISSN
- 18838189
- 04534654
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- NDL書誌ID
- 024320998
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- 本文言語コード
- en
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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