DC Field | Value | Language |
---|---|---|
dc.contributor.author | 박창수 | ko |
dc.contributor.author | 허종 | ko |
dc.contributor.author | 탁민제 | ko |
dc.date.accessioned | 2013-02-27T23:21:10Z | - |
dc.date.available | 2013-02-27T23:21:10Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 1999-01 | - |
dc.identifier.citation | 한국항공우주학회지, v.27, no.4, pp.104 - 114 | - |
dc.identifier.issn | 1225-1348 | - |
dc.identifier.uri | http://hdl.handle.net/10203/71455 | - |
dc.description.abstract | An aircraft acceleration control system is designed using various evolutionary algorithms. Evolution strategies are used to find the optimal gains for the controller. We also apply co-evolutionary algorithm in finding the saddle point solutions for the same system. Worst-case evolutionary algorithm is proposed for designing a robust controller. In the proposed algorithm, one group co-evolves while the other group simulates a random behavior. The evolving group is able to find a robust value for the search space. The solutions and properties of three methods are compared and analyzed. | - |
dc.language | Korean | - |
dc.publisher | 한국항공우주학회 | - |
dc.title | 진화 알고리듬을 이용한 항공기 제어기 설계 | - |
dc.title.alternative | Aircraft Control System Design Using Evolutionary Algorithm | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 27 | - |
dc.citation.issue | 4 | - |
dc.citation.beginningpage | 104 | - |
dc.citation.endingpage | 114 | - |
dc.citation.publicationname | 한국항공우주학회지 | - |
dc.contributor.localauthor | 탁민제 | - |
dc.contributor.nonIdAuthor | 박창수 | - |
dc.contributor.nonIdAuthor | 허종 | - |
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