Time-to-go Polynomial Guidance with Trajectory Modulation for Observability Enhancement

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dc.contributor.authorKim, Tae-Hunko
dc.contributor.authorLee, Chang-Hunko
dc.contributor.authorTahk, Min-Jeako
dc.date.accessioned2013-08-08T05:46:33Z-
dc.date.available2013-08-08T05:46:33Z-
dc.date.created2013-02-28-
dc.date.created2013-02-28-
dc.date.created2013-02-28-
dc.date.issued2013-01-
dc.identifier.citationIEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.49, no.1, pp.55 - 73-
dc.identifier.issn0018-9251-
dc.identifier.urihttp://hdl.handle.net/10203/174617-
dc.description.abstractA new impact angle control guidance law is introduced for a homing missile system equipped with a passive seeker against a stationary or slowly moving target. The proposed guidance law provides sufficient trajectory modulations, such as oscillatory trajectories, to enhance target observability from angle-only measurements. The derivation of the guidance command is based on the time-to-go polynomial guidance (TPG) law, which is one of the impact angle control laws. Closed-form solutions of the proposed law and their characteristics are investigated. The results inspired the proposed practical time-to-go calculation method and the maximum bounds of guidance gains, which are important for the practical implementation of the guidance law. Linear and nonlinear simulations with a target tracking filter are performed to investigate the performance of the proposed law.-
dc.languageEnglish-
dc.publisherIEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC-
dc.titleTime-to-go Polynomial Guidance with Trajectory Modulation for Observability Enhancement-
dc.typeArticle-
dc.identifier.wosid000313687000005-
dc.identifier.scopusid2-s2.0-84872242132-
dc.type.rimsART-
dc.citation.volume49-
dc.citation.issue1-
dc.citation.beginningpage55-
dc.citation.endingpage73-
dc.citation.publicationnameIEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS-
dc.contributor.localauthorLee, Chang-Hun-
dc.contributor.localauthorTahk, Min-Jea-
dc.description.isOpenAccessN-
dc.type.journalArticleArticle-
dc.subject.keywordPlusDUAL-CONTROL GUIDANCE-
dc.subject.keywordPlusHOMING MISSILES-
dc.subject.keywordPlusIMPACT-
dc.subject.keywordPlusCONSTRAINT-
dc.subject.keywordPlusLAW-
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AE-Journal Papers(저널논문)
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