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| ファイル | 記述 | サイズ | フォーマット | |
|---|---|---|---|---|
| mfeku_26_4_317.pdf | 474.36 kB | Adobe PDF | 見る/開く |
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| DCフィールド | 値 | 言語 |
|---|---|---|
| dc.contributor.author | MAEDA, Hiroshi | en |
| dc.date.accessioned | 2023-03-28T09:05:55Z | - |
| dc.date.available | 2023-03-28T09:05:55Z | - |
| dc.date.issued | 1964-10-27 | - |
| dc.identifier.uri | http://hdl.handle.net/2433/280606 | - |
| dc.description.abstract | A systematic and numerical procedure is described for optimizing the stability of a linear dynamic system. The process is an application of the so-called “steepest-descent method”, and since the stability of a linear dynamic system is determined by the real part of the roots of the characteristic equation, the practical procedure is suggested in this paper. A numerical example is presented for maximizing the damping of the perturbed motion of a earth satellite by the use of the gravity-oriented principle. | 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 to Optimize the Stability of a Linear Dynamic System | 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 | 26 | - |
| dc.identifier.issue | 4 | - |
| dc.identifier.spage | 317 | - |
| dc.identifier.epage | 327 | - |
| dc.textversion | publisher | - |
| dc.sortkey | 05 | - |
| 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.26 Part 4 | |
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