書誌事項
- タイトル別名
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- LQI based position control of a quad tilt-rotor UAV
抄録
<p>A quad tilt-rotor UAV is a UAV which has capability of independent position and attitude flight by adding actuators to change the thrust direction. However, since the number of actuators increases, the control system becomes complicated. It induces difficulty of gain adjustment for stable flight. In this research, focusing on position control, we aim to develop a control system that does not require trial and error gain adjustment for the quad tilt-rotor UAV, and evaluate its validity with numerical simulation and flight experiment.</p>
収録刊行物
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- ロボティクス・メカトロニクス講演会講演概要集
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ロボティクス・メカトロニクス講演会講演概要集 2019 (0), 1P1-N02-, 2019
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
- 1390283659833959808
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- NII論文ID
- 130007774352
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- ISSN
- 24243124
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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
- KAKEN
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- 抄録ライセンスフラグ
- 使用不可