DC Field | Value | Language |
---|---|---|
dc.contributor.author | Lee, Chang-Hun | ko |
dc.contributor.author | Kim, Tae-Hun | ko |
dc.contributor.author | Tahk, Min-Jea | ko |
dc.date.accessioned | 2014-08-29T01:44:23Z | - |
dc.date.available | 2014-08-29T01:44:23Z | - |
dc.date.created | 2014-03-03 | - |
dc.date.created | 2014-03-03 | - |
dc.date.created | 2014-03-03 | - |
dc.date.created | 2014-03-03 | - |
dc.date.issued | 2014-01 | - |
dc.identifier.citation | TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, v.57, no.1, pp.9 - 20 | - |
dc.identifier.issn | 0549-3811 | - |
dc.identifier.uri | http://hdl.handle.net/10203/188852 | - |
dc.description.abstract | This paper deals with a nonlinear adaptive autopilot design for agile missile systems. During the agile turn, there exist highly nonlinear, rapidly changing dynamics and aerodynamic uncertainties. To handle these difficulties, we propose a longitudinal autopilot for angle-of-attack tracking based on backstepping control methodology in conjunction with the time-delay adaptation scheme. The performance of the proposed method is investigated through nonlinear 6-DOF simulations using a reference angle-of-attack profile of agile turn that is obtained from trajectory optimization. An intercept scenario is performed to explore the applicability of the proposed control methodology to agile missile systems. | - |
dc.language | English | - |
dc.publisher | JAPAN SOC AERONAUT SPACE SCI | - |
dc.title | Agile Missile Autopilot Design using Nonlinear Backstepping Control with Time-Delay Adaptation | - |
dc.type | Article | - |
dc.identifier.wosid | 000330503600002 | - |
dc.identifier.scopusid | 2-s2.0-84892738232 | - |
dc.type.rims | ART | - |
dc.citation.volume | 57 | - |
dc.citation.issue | 1 | - |
dc.citation.beginningpage | 9 | - |
dc.citation.endingpage | 20 | - |
dc.citation.publicationname | TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | - |
dc.contributor.localauthor | Lee, Chang-Hun | - |
dc.contributor.localauthor | Tahk, Min-Jea | - |
dc.contributor.nonIdAuthor | Kim, Tae-Hun | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | Agile Missile | - |
dc.subject.keywordAuthor | Missile Autopilot | - |
dc.subject.keywordAuthor | Backstepping Control | - |
dc.subject.keywordAuthor | Adaptive Control | - |
dc.subject.keywordAuthor | Time-Delay Adaptation | - |
dc.subject.keywordPlus | OF-ATTACK MISSILE | - |
dc.subject.keywordPlus | HIGH-ANGLE | - |
dc.subject.keywordPlus | DISTURBANCE OBSERVER | - |
dc.subject.keywordPlus | ROBUST AUTOPILOT | - |
dc.subject.keywordPlus | NEURAL-NETWORKS | - |
dc.subject.keywordPlus | MOTION CONTROL | - |
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