DC FieldValueLanguage
dc.contributor.authorRosero García, Esteban Emilio-
dc.contributor.authorWerner, Herbert-
dc.date.accessioned2023-01-24T16:27:43Z-
dc.date.available2023-01-24T16:27:43Z-
dc.date.issued2014-10-
dc.identifier.citationUKACC International Conference on Control (CONTROL 2014)de_DE
dc.identifier.isbn9781479950119de_DE
dc.identifier.urihttp://hdl.handle.net/11420/14654-
dc.description.abstractIn this paper and its companion paper [16], the problem of cooperative source seeking by a formation of mobile agents is considered. Each agent is equipped with position and signal strength measurement sensors; their task is to find the maximum of the scalar field. Agents exchange information with neighboring agents through a communication network. In the first paper, a distributed gradient estimation for each agent and a decentralized navigation controller for single- and double-integrator models are presented. In this paper, that approach is extended to general linear time-invariant (LTI) models. Our approach is verified using formation flight simulation for quad-rotor helicopters and stability conditions are provided.en
dc.language.isoende_DE
dc.titleCooperative source seeking via gradient estimation and formation control (Part 2)de_DE
dc.typeinProceedingsde_DE
dc.type.dinicontributionToPeriodical-
dcterms.DCMITypeText-
tuhh.abstract.englishIn this paper and its companion paper [16], the problem of cooperative source seeking by a formation of mobile agents is considered. Each agent is equipped with position and signal strength measurement sensors; their task is to find the maximum of the scalar field. Agents exchange information with neighboring agents through a communication network. In the first paper, a distributed gradient estimation for each agent and a decentralized navigation controller for single- and double-integrator models are presented. In this paper, that approach is extended to general linear time-invariant (LTI) models. Our approach is verified using formation flight simulation for quad-rotor helicopters and stability conditions are provided.de_DE
tuhh.publisher.doi10.1109/CONTROL.2014.6915213-
tuhh.publication.instituteRegelungstechnik E-14de_DE
tuhh.type.opusInProceedings (Aufsatz / Paper einer Konferenz etc.)-
dc.type.drivercontributionToPeriodical-
dc.type.casraiConference Paper-
tuhh.container.startpage634de_DE
tuhh.container.endpage639de_DE
dc.relation.conferenceUKACC International Conference on Control, CONTROL 2014de_DE
dc.identifier.scopus2-s2.0-84921448336-
tuhh.container.articlenumber6915213de_DE
datacite.resourceTypeGeneralConferencePaper-
item.mappedtypeinProceedings-
item.fulltextNo Fulltext-
item.creatorGNDRosero García, Esteban Emilio-
item.creatorGNDWerner, Herbert-
item.openairecristypehttp://purl.org/coar/resource_type/c_5794-
item.cerifentitytypePublications-
item.grantfulltextnone-
item.languageiso639-1en-
item.creatorOrcidRosero García, Esteban Emilio-
item.creatorOrcidWerner, Herbert-
item.openairetypeinProceedings-
crisitem.author.deptRegelungstechnik E-14-
crisitem.author.orcid0000-0003-3456-5539-
crisitem.author.parentorgStudiendekanat Elektrotechnik, Informatik und Mathematik (E)-
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