DC Field | Value | Language |
---|---|---|
dc.contributor.author | Kim, Young-Sam | ko |
dc.contributor.author | Tahk, Min-Jea | ko |
dc.date.accessioned | 2019-10-08T07:20:08Z | - |
dc.date.available | 2019-10-08T07:20:08Z | - |
dc.date.created | 2019-10-07 | - |
dc.date.issued | 2019-10 | - |
dc.identifier.citation | PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.233, no.13, pp.4864 - 4878 | - |
dc.identifier.issn | 0954-4100 | - |
dc.identifier.uri | http://hdl.handle.net/10203/267836 | - |
dc.description.abstract | Landing is the most dangerous phase of the entire flight phases. If the total loss of thrust occurs during flight, a powered aircraft converts to a glider, which can use kinetic and potential energy only. For this reason, a proper scheme is needed for safe landing in cases of the total loss of thrust. This paper presents three-dimensional unpowered auto-landing guidance based on trajectory generation, expanding the concept of the energy-to-range ratio. We develop the terminal velocity estimation method for a horizontal plane applied to three-dimensional space; this method is based on the previously suggested terminal velocity estimation method for a vertical plane. Then, we show trajectory generation for landing guidance combining vertical with horizontal waypoints. The proposed auto-landing guidance with trajectory generation is evaluated by numerical simulation. | - |
dc.language | English | - |
dc.publisher | SAGE PUBLICATIONS LTD | - |
dc.title | Auto-landing guidance for unmanned aerial vehicle with engine flame-out | - |
dc.type | Article | - |
dc.identifier.wosid | 000483493400015 | - |
dc.identifier.scopusid | 2-s2.0-85061974345 | - |
dc.type.rims | ART | - |
dc.citation.volume | 233 | - |
dc.citation.issue | 13 | - |
dc.citation.beginningpage | 4864 | - |
dc.citation.endingpage | 4878 | - |
dc.citation.publicationname | PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | - |
dc.identifier.doi | 10.1177/0954410019831501 | - |
dc.contributor.localauthor | Tahk, Min-Jea | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | Unmanned air vehicle | - |
dc.subject.keywordAuthor | landing guidance | - |
dc.subject.keywordAuthor | auto-landing | - |
dc.subject.keywordAuthor | total loss of thrust | - |
dc.subject.keywordAuthor | unpowered landing | - |
dc.subject.keywordAuthor | terminal velocity estimation | - |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.