DC Field | Value | Language |
---|---|---|
dc.contributor.author | Cho, HJ | ko |
dc.contributor.author | Ryoo, CK | ko |
dc.contributor.author | Tahk, Min-Jea | ko |
dc.date.accessioned | 2013-03-03T00:19:32Z | - |
dc.date.available | 2013-03-03T00:19:32Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 1996-09 | - |
dc.identifier.citation | JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.19, no.5, pp.1017 - 1022 | - |
dc.identifier.issn | 0731-5090 | - |
dc.identifier.uri | http://hdl.handle.net/10203/76211 | - |
dc.description.abstract | An optimal guidance law for missiles with time-varying velocity is investigated. The closed-form solution is derived and properties of the key variables of the solution, such as a time-to-go-like function and the time-varying guidance gain, are studied, Implementation aspects related to the computations of time-to-go and the guidance gain also are considered. Simulation studies show that the performance of the proposed guidance law is superior to that of proportional navigation or augmented proportional navigation. | - |
dc.language | English | - |
dc.publisher | AMER INST AERONAUT ASTRONAUT | - |
dc.title | Closed-form optimal guidance law for missiles of time-varying velocity | - |
dc.type | Article | - |
dc.identifier.wosid | A1996VE51300005 | - |
dc.identifier.scopusid | 2-s2.0-0030242427 | - |
dc.type.rims | ART | - |
dc.citation.volume | 19 | - |
dc.citation.issue | 5 | - |
dc.citation.beginningpage | 1017 | - |
dc.citation.endingpage | 1022 | - |
dc.citation.publicationname | JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | - |
dc.contributor.localauthor | Tahk, Min-Jea | - |
dc.contributor.nonIdAuthor | Cho, HJ | - |
dc.contributor.nonIdAuthor | Ryoo, CK | - |
dc.type.journalArticle | Article | - |
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