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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 | 2023-03-28T09:05:57Z | - |
dc.date.available | 2023-03-28T09:05:57Z | - |
dc.date.issued | 1965-05-20 | - |
dc.identifier.uri | http://hdl.handle.net/2433/280623 | - |
dc.description.abstract | A numerical method to optimize the stability of a linear dynamic system which was described in the last paper is generalized to the case of equality constraints in this report. The process is an application of the “steepest-descent method” as well, and it is inclusive of the procedure given in the last paper as a simple case. Hence, with application of this method, problems which are of practical interest but are difficult to treat with the previous method are expected to be solvable. A numerical example is presented for maximizing the damping of the Dutch-Roll mode of motion of an 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 to Optimize the Stability of a Linear Dynamic System : II. With Equality Constraints | 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 | 27 | - |
dc.identifier.issue | 2 | - |
dc.identifier.spage | 166 | - |
dc.identifier.epage | 177 | - |
dc.textversion | publisher | - |
dc.sortkey | 03 | - |
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.27 Part 2 |
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