書誌事項
- タイトル別名
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- Design and performance verification of the reference trajectory and the control system for the hammer-head turn flight maneuver of unmanned helicopters
抄録
<p>Designing a control system and a reference trajectory for a small single-rotor helicopter for flight control of a hammer head turn with a load of 2G or more, a vertical attitude and a non-thrusting flight state from a high-speed straight flight, and verification by flight experiments went. In the control system design, a control law for velocity compensation near the reference trajectory in a flight with no thrust was implemented. The reference trajectory was designed as a periodic function of the nose vertical angle using the monotonicity of the attitude change in order to design an asymmetric thrust trajectory in ascent and descent.</p>
収録刊行物
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- 日本機械学会関東支部総会講演会講演論文集
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日本機械学会関東支部総会講演会講演論文集 2020 (0), 16C01-, 2020-03-13
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
- 1390568772521919872
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- NII論文ID
- 130007994412
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- ISSN
- 24242691
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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