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mfeku_23_2_154.pdf | 4.21 MB | Adobe PDF | 見る/開く |
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DCフィールド | 値 | 言語 |
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dc.contributor.author | MAEDA, Hiroshi | en |
dc.date.accessioned | 2023-03-28T09:05:36Z | - |
dc.date.available | 2023-03-28T09:05:36Z | - |
dc.date.issued | 1961-05-31 | - |
dc.identifier.uri | http://hdl.handle.net/2433/280495 | - |
dc.description.abstract | A method of treating a human-piloted airplane as one closed-loop system and calculating the dynamic stability of the airplane by the Evans's “Root-Locus Method” has been investigated. Using this method, not only the characteristics of the transient motion but also the control ability of the human-pilot to decrease the residual motion of the airplane can be understood conveniently. In this paper, some results of numerical calculation with this method are described for a typical airplane. | en |
dc.language.iso | eng | - |
dc.publisher | Faculty of Engineering, Kyoto University | en |
dc.publisher.alternative | 京都大学工学部 | ja |
dc.subject.ndc | 500 | - |
dc.title | A Method for Calculating the Dynamic Stability of a Human-Piloted Airplane by the “Root-Locus Method” | en |
dc.type | departmental bulletin paper | - |
dc.type.niitype | Departmental Bulletin Paper | - |
dc.identifier.ncid | AA00732503 | - |
dc.identifier.jtitle | Memoirs of the Faculty of Engineering, Kyoto University | en |
dc.identifier.volume | 23 | - |
dc.identifier.issue | 2 | - |
dc.identifier.spage | 154 | - |
dc.identifier.epage | 171 | - |
dc.textversion | publisher | - |
dc.sortkey | 04 | - |
dc.address | Department of Aeronautical Engineering | en |
dcterms.accessRights | open access | - |
dc.identifier.pissn | 0023-6063 | - |
出現コレクション: | Vol.23 Part 2 |

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