DC Field | Value | Language |
---|---|---|
dc.contributor.author | Kim, Sang Hwa | ko |
dc.contributor.author | Tahk, Min-Jea | ko |
dc.contributor.author | Lee, Ha-Jun | ko |
dc.contributor.author | Kim, Seung-Hwan | ko |
dc.date.accessioned | 2016-09-07T04:23:51Z | - |
dc.date.available | 2016-09-07T04:23:51Z | - |
dc.date.created | 2016-08-29 | - |
dc.date.created | 2016-08-29 | - |
dc.date.issued | 2016-06 | - |
dc.identifier.citation | IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.52, no.3, pp.1467 - U569 | - |
dc.identifier.issn | 0018-9251 | - |
dc.identifier.uri | http://hdl.handle.net/10203/212879 | - |
dc.description.abstract | This paper describes an experimental study on an integrated servo control method. Conventional servo control schemes may experience performance degradation under the presence of physical constraints. An integrated scheme is proposed in this study to address this problem. In the proposed method, three controllers correspond to autopilot commands directly instead of four actuators. Various simulations and experiments show that the proposed integrated servo control method provides better performance than the conventional ones | - |
dc.language | English | - |
dc.publisher | IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC | - |
dc.subject | ELECTROMECHANICAL FLIGHT ACTUATORS | - |
dc.title | Experimental Study on Integrated Servo Control for Canard-Controlled Missiles | - |
dc.type | Article | - |
dc.identifier.wosid | 000380113800040 | - |
dc.identifier.scopusid | 2-s2.0-84979941619 | - |
dc.type.rims | ART | - |
dc.citation.volume | 52 | - |
dc.citation.issue | 3 | - |
dc.citation.beginningpage | 1467 | - |
dc.citation.endingpage | U569 | - |
dc.citation.publicationname | IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | - |
dc.identifier.doi | 10.1109/TAES.2016.150211 | - |
dc.contributor.localauthor | Tahk, Min-Jea | - |
dc.contributor.nonIdAuthor | Lee, Ha-Jun | - |
dc.contributor.nonIdAuthor | Kim, Seung-Hwan | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordPlus | ELECTROMECHANICAL FLIGHT ACTUATORS | - |
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