Publication:
Hybrid Optimal Control for Aircraft Trajectory Design with a Variable Sequence of Modes

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dc.affiliation.dptoUC3M. Departamento de Ingeniería Aeroespaciales
dc.affiliation.grupoinvUC3M. Grupo de Investigación: Ingeniería Aeroespaciales
dc.contributor.authorKamgarpour, Maryam
dc.contributor.authorSoler, Manueles
dc.contributor.authorTomlin, Claire J.
dc.contributor.authorOlivares, Alberto
dc.contributor.authorLygeros, John
dc.date.accessioned2015-06-11T10:16:08Z
dc.date.available2015-06-11T10:16:08Z
dc.date.issued2011
dc.descriptionProceedings of: 18th World Congress of the International Federation of Automatic Control (IFAC). Milan, 29 August - 02 September 2011.en
dc.description.abstractThe problem of aircraft trajectory planning is formulated as a hybrid optimal control problem. The aircraft is modeled as a switched system, that is, a class of hybrid dynamical systems. The sequence of modes, the switching times, and the inputs for each mode are the control variables. An iterative bi-level optimization algorithm is employed to solve the optimal control problem. At the lower level, given a pre-de ned sequence of ight modes, the optimal switching times and the input for each mode are determined. This is achieved by extending the continuous state to include the switching times and then solving a conventional optimal control problem for the extended state. At the higher level, the algorithm modi es the mode sequence in order to decrease the value of the cost function. We illustrate the utility of the problem formulation and the solution approach with two case studies in which short horizon aircraft trajectories are optimized in order to reduce fuel burn while avoiding hazardous weather.en
dc.description.sponsorshipThis work was partially supported by AFOSR under grant FA9550-06-1-0312 and by the National Science and Engineering Research Council of Canada (NSERC); by the Spanish Government under ATLANTIDA project, and the European Union's FP7 for the Clean Sky JTI under grant 270624; and the European Commission under the project iFly, FP6-TREN-037180.en
dc.description.statusPublicadoes
dc.format.extent6es
dc.format.mimetypeapplication/pdf
dc.identifier.bibliographicCitationBittanti, S. et al. (eds.) (2011). Proceedings of the 18th IFAC World Congress, 2011. (pp. 7238-7243). International Federation of Automatic Control.en
dc.identifier.doi10.3182/20110828-6-IT-1002.01643
dc.identifier.isbn978-3-902661-93-7
dc.identifier.issn1474-6670
dc.identifier.publicationfirstpage7238
dc.identifier.publicationlastpage7243
dc.identifier.publicationtitleProceedings of the 18th IFAC World Congressen
dc.identifier.publicationvolume1
dc.identifier.urihttps://hdl.handle.net/10016/21068
dc.identifier.uxxiCC/0000020601
dc.language.isoeng
dc.publisherIfac Papers Onlineen
dc.relation.eventdate29 August - 02 September 2011.en
dc.relation.eventnumber18
dc.relation.eventplaceMilán, Italiaen
dc.relation.eventtitle18th World Congress of the International Federation of Automatic Control (IFAC)en
dc.relation.ispartofseriesWorld Congressen
dc.relation.ispartofseries18
dc.relation.projectIDinfo:eu-repo/grantAgreement/EC/FP7/270624en
dc.relation.publisherversionhttp://dx.doi.org/10.3182/20110828-6-IT-1002.01643en
dc.rights© 2011 International Federation of Automatic Control (IFAC)es
dc.rights.accessRightsopen accessen
dc.subject.ecienciaAeronáuticaes
dc.subject.otherOptimal Controlen
dc.subject.otherHybrid Systemsen
dc.subject.otherAircraft Operationsen
dc.subject.otherAircraft Trajectory Designen
dc.titleHybrid Optimal Control for Aircraft Trajectory Design with a Variable Sequence of Modesen
dc.typeconference paper*
dc.type.hasVersionAM*
dspace.entity.typePublication
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