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Development of tailless two-winged flapping drone with gravity center position control
http://hdl.handle.net/10069/00040873
http://hdl.handle.net/10069/000408734b3c67f6-594e-443c-a3de-3ffd872f32b1
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
SenMet33_859.pdf (2.4 MB)
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| Item type | 学術雑誌論文 / Journal Article(1) | |||||
|---|---|---|---|---|---|---|
| 公開日 | 2021-09-10 | |||||
| タイトル | ||||||
| タイトル | Development of tailless two-winged flapping drone with gravity center position control | |||||
| 言語 | ||||||
| 言語 | eng | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | flapping wing | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | micro air vehicle | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | autonomous flight | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | biomimetics | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | flexible structure | |||||
| 資源タイプ | ||||||
| 資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
| 資源タイプ | journal article | |||||
| 著者 |
Nagai, Hiroto
× Nagai, Hiroto× Nakamura, Kazutaka× Fujita, Koki× Tanaka, Issei× Nagasaki, Shuji× Kinjo, Yutaka× Kuwazono, Shintaro× Murozono, Masahiko |
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| 抄録 | ||||||
| 内容記述タイプ | Abstract | |||||
| 内容記述 | We have developed a tailless, two-winged flapping drone with a full span length of 180 mm and a total weight of 20.5 g. The developed flapping drone is characterized by three biomimetic techniques: an anisotropic vein pattern reinforcing the wing surfaces, an elastic flapping mechanism, and gravity center position control in the abdomen. On the basis of experimental and numerical results, the flapping wings are reinforced by a vein pattern made of an anisotropic carbon fiber-reinforced plastic (CFRP) laminate to passively provide appropriate aeroelastic deformation and positively utilize snap-though buckling on the wing surface at stroke reversals to provide a fast feathering rotation. The flapping wing kinematics are provided by a novel flapping mechanism with an energy recovery system using the elasticity of the mechanical system. Unlike other previously developed flapping robots, feedback control to stabilize the pitch and roll angles of the drone’s body is conducted using a technique of gravity center position control, where the tail angles of the body are changed similarly to the abdominal movements of insects in flight. The developed flapping drone has succeeded in an autonomous hovering flight for more than 30 s and a vertical take-off under a wireless condition with the gravity center position control. | |||||
| 書誌情報 |
Sensors and Materials 巻 33, 号 3, p. 859-872, 発行日 2021-03-05 |
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| 出版者 | ||||||
| 出版者 | M Y U Scientific Publishing Division | |||||
| ISSN | ||||||
| 収録物識別子タイプ | ISSN | |||||
| 収録物識別子 | 0914-4935 | |||||
| EISSN | ||||||
| 収録物識別子タイプ | ISSN | |||||
| 収録物識別子 | 2435-0869 | |||||
| DOI | ||||||
| 関連タイプ | isIdenticalTo | |||||
| 識別子タイプ | DOI | |||||
| 関連識別子 | 10.18494/SAM.2021.3222 | |||||
| 権利 | ||||||
| 権利情報 | c 2021 M Y U Scientific Publishing Division. This work is licensed under a Creative Commons Attribution 4.0 International License. Sensors and Materials, 33(3), pp. 859-872; 2021, and DOI:10.18494/SAM.2021.3222 | |||||
| 著者版フラグ | ||||||
| 出版タイプ | VoR | |||||
| 出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
| 引用 | ||||||
| 内容記述タイプ | Other | |||||
| 内容記述 | Sensors and Materials, 33(3), pp. 859-872; 2021 | |||||
