유연구조 발사체의 고전구조 자세제어기 최적설계Optimal Design of the Classical-Type Attitude Controller for a Flexible Launch Vehicle
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | 허종 | ko |
| dc.contributor.author | 송은정 | ko |
| dc.contributor.author | 탁민제 | ko |
| dc.date.accessioned | 2013-02-28T02:24:09Z | - |
| dc.date.available | 2013-02-28T02:24:09Z | - |
| dc.date.created | 2012-02-06 | - |
| dc.date.created | 2012-02-06 | - |
| dc.date.issued | 1998-01 | - |
| dc.identifier.citation | 한국항공우주학회지, v.26, no.7, pp.96 - 107 | - |
| dc.identifier.issn | 1225-1348 | - |
| dc.identifier.uri | http://hdl.handle.net/10203/72271 | - |
| dc.language | Korean | - |
| dc.publisher | 한국항공우주학회 | - |
| dc.title | 유연구조 발사체의 고전구조 자세제어기 최적설계 | - |
| dc.title.alternative | Optimal Design of the Classical-Type Attitude Controller for a Flexible Launch Vehicle | - |
| dc.type | Article | - |
| dc.type.rims | ART | - |
| dc.citation.volume | 26 | - |
| dc.citation.issue | 7 | - |
| dc.citation.beginningpage | 96 | - |
| dc.citation.endingpage | 107 | - |
| dc.citation.publicationname | 한국항공우주학회지 | - |
| dc.contributor.localauthor | 탁민제 | - |
| dc.contributor.nonIdAuthor | 허종 | - |
| dc.contributor.nonIdAuthor | 송은정 | - |
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