충돌각 제약조건을 고려한 순간낙하점 기반의 중기 유도 기법Midcourse Guidance laws based on Instantaneous Impact Point considering Final Impact Angle Constraint
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | 황준섭 | ko |
| dc.contributor.author | 안재명 | ko |
| dc.date.accessioned | 2021-07-22T00:10:22Z | - |
| dc.date.available | 2021-07-22T00:10:22Z | - |
| dc.date.created | 2021-07-21 | - |
| dc.date.issued | 2021-07-09 | - |
| dc.identifier.citation | 한국항공우주학회 2021년도 춘계학술대회 | - |
| dc.identifier.uri | http://hdl.handle.net/10203/286798 | - |
| dc.language | Korean | - |
| dc.publisher | 한국항공우주학회 | - |
| dc.title | 충돌각 제약조건을 고려한 순간낙하점 기반의 중기 유도 기법 | - |
| dc.title.alternative | Midcourse Guidance laws based on Instantaneous Impact Point considering Final Impact Angle Constraint | - |
| dc.type | Conference | - |
| dc.type.rims | CONF | - |
| dc.citation.publicationname | 한국항공우주학회 2021년도 춘계학술대회 | - |
| dc.identifier.conferencecountry | KO | - |
| dc.identifier.conferencelocation | 쏠비치 삼척 | - |
| dc.contributor.localauthor | 안재명 | - |
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