DC Field | Value | Language |
---|---|---|
dc.contributor.author | Song, EJ | ko |
dc.contributor.author | Tahk, Min-Jea | ko |
dc.date.accessioned | 2013-03-02T16:48:42Z | - |
dc.date.available | 2013-03-02T16:48:42Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 1998-08 | - |
dc.identifier.citation | CONTROL ENGINEERING PRACTICE, v.6, no.8, pp.957 - 967 | - |
dc.identifier.issn | 0967-0661 | - |
dc.identifier.uri | http://hdl.handle.net/10203/74526 | - |
dc.description.abstract | In this paper, an on-line suboptimal midcourse guidance law, which is a neural-network approximation of the optimal feedback strategy, is proposed to eliminate the need for solving two-point boundary-value problems in real time. Moreover, for intercept point prediction, a fast converging, iterative algorithm based on a neural network time-to-go estimator is devised. Computer simulations confirm that the closed-loop behavior of the proposed guidance law is so close to the optimal trajectory that it outperforms nonoptimal guidance laws such as g-biased proportional navigation. (C) 1998 Elsevier Science Ltd. All rights reserved. | - |
dc.language | English | - |
dc.publisher | PERGAMON-ELSEVIER SCIENCE LTD | - |
dc.subject | TO-AIR MISSILES | - |
dc.title | Real-time midcourse guidance with intercept point prediction | - |
dc.type | Article | - |
dc.identifier.wosid | 000077551600004 | - |
dc.identifier.scopusid | 2-s2.0-0032131110 | - |
dc.type.rims | ART | - |
dc.citation.volume | 6 | - |
dc.citation.issue | 8 | - |
dc.citation.beginningpage | 957 | - |
dc.citation.endingpage | 967 | - |
dc.citation.publicationname | CONTROL ENGINEERING PRACTICE | - |
dc.contributor.localauthor | Tahk, Min-Jea | - |
dc.contributor.nonIdAuthor | Song, EJ | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | midcourse guidance | - |
dc.subject.keywordAuthor | suboptimal feedback law | - |
dc.subject.keywordAuthor | optimal trajectory | - |
dc.subject.keywordAuthor | neural networks | - |
dc.subject.keywordAuthor | iterative prediction algorithms | - |
dc.subject.keywordPlus | TO-AIR MISSILES | - |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.