Autopilot design synthesis for highly maneuverable STT(Skid-To-Turn) missiles고기동 STT 유도탄의 오토파일롯 설계기법 연구
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.advisor | Tahk, Min-Jea | - |
| dc.contributor.advisor | 탁민제 | - |
| dc.contributor.author | Kim, Seung-Hwan | - |
| dc.contributor.author | 김승환 | - |
| dc.date.accessioned | 2013-09-11 | - |
| dc.date.available | 2013-09-11 | - |
| dc.date.issued | 2012 | - |
| dc.identifier.uri | http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=487162&flag=dissertation | - |
| dc.identifier.uri | http://hdl.handle.net/10203/179633 | - |
| dc.description | 학위논문(박사) - 한국과학기술원 : 항공우주공학전공, 2012.2, [ vi, 126 p. ] | - |
| dc.language | eng | - |
| dc.publisher | 한국과학기술원 | - |
| dc.subject | autopilot design | - |
| dc.subject | Highly maneuverable STT missile | - |
| dc.subject | nonlinear dynamic control | - |
| dc.subject | aerodynamic coupling modeling | - |
| dc.subject | 고기동 STT 미사일 | - |
| dc.subject | 오토파일롯 설계 | - |
| dc.subject | 비선형 동적제어기 | - |
| dc.subject | 공력학적 커플링 모델링 | - |
| dc.subject | 새로운 구조의 구동제어시스템 | - |
| dc.subject | new structure of actuation control system | - |
| dc.title | Autopilot design synthesis for highly maneuverable STT(Skid-To-Turn) missiles | - |
| dc.title.alternative | 고기동 STT 유도탄의 오토파일롯 설계기법 연구 | - |
| dc.type | Thesis(Ph.D) | - |
| dc.identifier.CNRN | 487162/325007 | - |
| dc.description.department | 한국과학기술원 : 항공우주공학전공, | - |
| dc.identifier.uid | 020085243 | - |
| dc.contributor.localauthor | Tahk, Min-Jea | - |
| dc.contributor.localauthor | 탁민제 | - |
- Appears in Collection
- AE-Theses_Ph.D.(박사논문)
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