書誌事項
- タイトル別名
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- Attitude Control System Design of Small-scale Airplanes
抄録
<p>An attitude control system design of a small aircraft is considered in the study. The attitude control system is designed based on the dynamic model of the aircraft in the vertical and horizontal directions. A gain scheduling control method considering the restriction of the elevator angle in the attitude control maneuver is proposed. The effectiveness of the present gain scheduling control is shown in the simulation study.</p>
収録刊行物
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- 北陸信越支部総会・講演会 講演論文集
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北陸信越支部総会・講演会 講演論文集 2017.54 (0), E011-, 2017
一般社団法人 日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1390001205865966080
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- NII論文ID
- 130007110605
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- ISSN
- 24242772
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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
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可