DC Field | Value | Language |
---|---|---|
dc.contributor.author | Oh, Gyeongtaek | ko |
dc.contributor.author | Park, Jongho | ko |
dc.contributor.author | Park, Jeongha | ko |
dc.contributor.author | Lee, Hongju | ko |
dc.contributor.author | Kim, Youdan | ko |
dc.contributor.author | Shin, Sang-Joon | ko |
dc.contributor.author | Ahn, Jaemyung | ko |
dc.contributor.author | Cho, Sangbum | ko |
dc.date.accessioned | 2018-06-16T07:20:59Z | - |
dc.date.available | 2018-06-16T07:20:59Z | - |
dc.date.created | 2017-02-02 | - |
dc.date.created | 2017-02-02 | - |
dc.date.created | 2017-02-02 | - |
dc.date.created | 2017-02-02 | - |
dc.date.issued | 2018-06 | - |
dc.identifier.citation | PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.232, no.8, pp.1598 - 1605 | - |
dc.identifier.issn | 0954-4100 | - |
dc.identifier.uri | http://hdl.handle.net/10203/242455 | - |
dc.description.abstract | A nonlinear closed-loop load relief scheme is proposed to reduce the aerodynamic load during the ascent phase of a launch vehicle. The proposed controller is designed based on a back-stepping and sliding-mode control scheme with aerodynamic angle feedback. A hybrid load-relief strategy using the load relief scheme around the period of the maximum dynamic pressure and the traditional minimum-drift scheme during the other period is proposed. An aerodynamic angle estimator is also developed using a Kalman filter for the feedback of the load relief control. Numerical simulation is conducted to demonstrate the performance of the proposed strategy as well as the potential benefits. | - |
dc.language | English | - |
dc.publisher | SAGE PUBLICATIONS LTD | - |
dc.title | Load relief control of launch vehicle using aerodynamic angle estimation | - |
dc.type | Article | - |
dc.identifier.wosid | 000433436100015 | - |
dc.identifier.scopusid | 2-s2.0-85045243634 | - |
dc.type.rims | ART | - |
dc.citation.volume | 232 | - |
dc.citation.issue | 8 | - |
dc.citation.beginningpage | 1598 | - |
dc.citation.endingpage | 1605 | - |
dc.citation.publicationname | PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | - |
dc.identifier.doi | 10.1177/0954410017699435 | - |
dc.contributor.localauthor | Ahn, Jaemyung | - |
dc.contributor.nonIdAuthor | Oh, Gyeongtaek | - |
dc.contributor.nonIdAuthor | Park, Jongho | - |
dc.contributor.nonIdAuthor | Park, Jeongha | - |
dc.contributor.nonIdAuthor | Lee, Hongju | - |
dc.contributor.nonIdAuthor | Kim, Youdan | - |
dc.contributor.nonIdAuthor | Shin, Sang-Joon | - |
dc.contributor.nonIdAuthor | Cho, Sangbum | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | Launch vehicle | - |
dc.subject.keywordAuthor | hybrid load relief control | - |
dc.subject.keywordAuthor | angle of attack estimation | - |
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