DC Field | Value | Language |
---|---|---|
dc.contributor.author | Kim, Iksoo | ko |
dc.contributor.author | Choi, Han-Lim | ko |
dc.contributor.author | Jeon, In-Soo | ko |
dc.date.accessioned | 2021-12-03T06:40:35Z | - |
dc.date.available | 2021-12-03T06:40:35Z | - |
dc.date.created | 2021-05-11 | - |
dc.date.created | 2021-05-11 | - |
dc.date.created | 2021-05-11 | - |
dc.date.created | 2021-05-11 | - |
dc.date.created | 2021-05-11 | - |
dc.date.issued | 2021-12 | - |
dc.identifier.citation | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.22, no.6, pp.1428 - 1439 | - |
dc.identifier.issn | 2093-274X | - |
dc.identifier.uri | http://hdl.handle.net/10203/289910 | - |
dc.description.abstract | This paper addresses an impact angle control guidance problem for nose-dive missiles to achieve the maximum terminal speed against a fixed target in the same vertical plane. By modeling the aerodynamic drag as a drag polar, we set up the nonlinear system equations needed to pursue an analytic closed-form solution. This paper shows that maximizing the terminal speed is equivalent to minimizing a weighted quadratic cost of the curvature of trajectory, and can be used as an equivalent problem to the original problem. Applying Pontryagin's maximum principle to the equivalent problem, we obtained a closed-form optimal guidance law, described in terms of air density parameters as well as heading error angle, flight path angle, range-to-go, and time-varying speed. | - |
dc.language | English | - |
dc.publisher | SPRINGER | - |
dc.title | Closed-Form Impact-Angle-Control Guidance of Nose-Dive Missiles for Maximum Terminal Speed | - |
dc.type | Article | - |
dc.identifier.wosid | 000638521100001 | - |
dc.identifier.scopusid | 2-s2.0-85104140551 | - |
dc.type.rims | ART | - |
dc.citation.volume | 22 | - |
dc.citation.issue | 6 | - |
dc.citation.beginningpage | 1428 | - |
dc.citation.endingpage | 1439 | - |
dc.citation.publicationname | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES | - |
dc.identifier.doi | 10.1007/s42405-021-00361-3 | - |
dc.embargo.liftdate | 9999-12-31 | - |
dc.embargo.terms | 9999-12-31 | - |
dc.identifier.kciid | ART002783769 | - |
dc.contributor.localauthor | Choi, Han-Lim | - |
dc.contributor.nonIdAuthor | Jeon, In-Soo | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | Impact angle control guidance | - |
dc.subject.keywordAuthor | Nose-dive missile | - |
dc.subject.keywordAuthor | Maximum terminal speed | - |
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