| タイトルヨミ | ヨンジク カイテンヨクガタ RC ヘリコプタ ノ カイハツ ニ カンスル キソテキ ケンキュウ 1 ホンキ ノ セイサク
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| 日本語以外のタイトル | Fundamental Studies on Development of Four-Rotor Type RC-Helicopter(Part 1) : Trial Production of RC-Helicopter
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| ファイル | |
| 言語 |
日本語
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| 著者 |
中尾 清治
吉田 忠彦
姚 剣亭
藤浦 建史
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| 内容記述（抄録等） | RC-helicopter that can be controlled easily may be required on use of farm work in future. In this paper, four-rotor type RC-helicopter was tried to develop and the results of some flight tests were reported.
The trial RC-helicopter had four rotors which were driven by DC motors, The pitch angle was fixed and the revolutional speed of each motor was controlled by way of PWM (pulse width modulation). They revoluted in the opposite direction each other in order to defeat the reaction torque of the body caused by the revolution of rotors. The flight stability of the RC-helicopter could be controlled automatically by two gyroscopes. From the test resullts, the best pitch angle of the rotor was 10 degrees. The maximum lifting force of trial RC-helicopter with the best pitch angle was 15.9 N at 1170 rpm in rotor revolution. |
| 掲載誌名 |
島根大学農学部研究報告
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| 巻 | 27
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| 開始ページ | 23
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| 終了ページ | 26
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| ISSN | 0370940X
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| 発行日 | 1993-12-20
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| NCID | AN00108015
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| 出版者 | 島根大学農学部
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| 出版者別表記 | Shimane University, Faculty of Agriculture
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| 資料タイプ |
紀要論文
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| 部局 |
生物資源科学部
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| 他の一覧 |
