A missile guidance law based on Sontags formula to intercept maneuvering targets

Cited 11 time in webofscience Cited 0 time in scopus
  • Hit : 537
  • Download : 0
DC FieldValueLanguage
dc.contributor.authorRyoo, Chang-Kyungko
dc.contributor.authorKim, Yoon-Hwanko
dc.contributor.authorTahk, Min-Jeako
dc.contributor.authorChoi, Keeyoungko
dc.date.accessioned2013-03-06T09:39:43Z-
dc.date.available2013-03-06T09:39:43Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued2007-08-
dc.identifier.citationINTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, v.5, no.4, pp.397 - 409-
dc.identifier.issn1598-6446-
dc.identifier.urihttp://hdl.handle.net/10203/86586-
dc.description.abstractIn this paper, we propose a nonlinear guidance law for missiles against maneuvering targets. First, we derive the equations of motion described in the line-of-sight reference frame and then we define the equilibrium subspace of the nonlinear system to guarantee target interception within a finite time. Using Sontag's formula, we derive a nonlinear guidance law that always delivers the state to the equilibrium subspace. If the speed of the missile is greater than that of the target, the proposed law has global capturability in that, under any initial launch conditions, the missile can intercept the maneuvering target. The proposed law also minimizes the integral cost of the control energy and the weighted square of the state. The performance of the proposed law is compared with the augmented proportional navigation guidance law by means of numerical simulations of various initial conditions and target maneuvers.-
dc.languageEnglish-
dc.publisherINST CONTROL ROBOTICS & SYSTEMS-
dc.subjectTRUE PROPORTIONAL NAVIGATION-
dc.subjectSTABILIZATION-
dc.subjectCAPTURABILITY-
dc.titleA missile guidance law based on Sontags formula to intercept maneuvering targets-
dc.typeArticle-
dc.identifier.wosid000248954500006-
dc.identifier.scopusid2-s2.0-34547622672-
dc.type.rimsART-
dc.citation.volume5-
dc.citation.issue4-
dc.citation.beginningpage397-
dc.citation.endingpage409-
dc.citation.publicationnameINTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS-
dc.contributor.localauthorTahk, Min-Jea-
dc.contributor.nonIdAuthorRyoo, Chang-Kyung-
dc.contributor.nonIdAuthorKim, Yoon-Hwan-
dc.contributor.nonIdAuthorChoi, Keeyoung-
dc.type.journalArticleArticle-
dc.subject.keywordAuthorcontrol Lyapunov function-
dc.subject.keywordAuthormissile guidance-
dc.subject.keywordAuthornonlinear control-
dc.subject.keywordAuthorSontag&apos-
dc.subject.keywordAuthors formula.-
dc.subject.keywordPlusTRUE PROPORTIONAL NAVIGATION-
dc.subject.keywordPlusSTABILIZATION-
dc.subject.keywordPlusCAPTURABILITY-
Appears in Collection
AE-Journal Papers(저널논문)
Files in This Item
There are no files associated with this item.
This item is cited by other documents in WoS
⊙ Detail Information in WoSⓡ Click to see webofscience_button
⊙ Cited 11 items in WoS Click to see citing articles in records_button

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0