Flight Characteristics of Quad Rotor Helicopter with Thrust Vectoring Equipment
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- Imamura Akitaka
- Osaka Sangyo University
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- Miwa Masafumi
- Tokushima University
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- Hino Junichi
- Tokushima University
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説明
<p>A quad rotor helicopter (QRH) is a radio controlled (RC) aircraft that tilts its attitude to generate a horizontal force component to move in a certain direction. Using autonomous control, the attitude control system tilts the airframe against disturbances, such as wind. Thus, the attitude of a flying QRH is always slanted. In this study, three types of deflecting thruster were compared to maintain the position and horizontal attitude of the QRH. The extra thrusters are tilted to generate a thrust against disturbances without causing the airframe to incline. It is suitable for precise measurements for which the airframe posture should remain horizontal.</p>
収録刊行物
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- Journal of Robotics and Mechatronics
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Journal of Robotics and Mechatronics 28 (3), 334-342, 2016-06-20
富士技術出版株式会社
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詳細情報 詳細情報について
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- CRID
- 1390282763126703360
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- NII論文ID
- 130007671019
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- NII書誌ID
- AA10809998
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- ISSN
- 18838049
- 09153942
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- NDL書誌ID
- 027568430
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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サーチ
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可