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dc.contributor.authorDiaz-Mercado, Yancy
dc.contributor.authorLee, Sung G.
dc.contributor.authorEgerstedt, Magnus B.
dc.contributor.authorYoung, Shih-Yih
dc.date.accessioned2014-10-15T22:52:30Z
dc.date.available2014-10-15T22:52:30Z
dc.date.issued2013-10
dc.identifier.citationY. Diaz-Mercado, S. Lee, M. Egerstedt, and S.Y. Young. Optimal Trajectory Generation for Next Generation Flight Management Systems. Digital Avionics Systems Conference, Syracuse, NY, Oct. 2013, pp. 3C5-1 - 3C5-10.en_US
dc.identifier.isbn978-1-4799-1536-1
dc.identifier.issn2155-7195
dc.identifier.urihttp://hdl.handle.net/1853/52655
dc.description© 2013 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.en_US
dc.descriptionPresented at the Digital Avionics Systems Conference, Syracuse, NY, Oct. 2013.
dc.descriptionDOI: 10.1109/DASC.2013.6712566
dc.description.abstractNext generation flight management systems require the compliance of temporal and spatial constraints on navigation performance. The problem of generating fuel-efficient trajectories for aircrafts that comply with the required navigation performance is approached from an optimal control framework. By deriving the necessary conditions for optimality, nominal optimal control signals can be generated in a computationally efficient manner. These control signals can be used to generate nominal trajectories for an aircraft model. Using the nominal control and nominal trajectory, a feedforward-feedback control scheme can be implemented to robustify the system’s response in the presence of uncertainty and disturbances to still achieve the required navigation performance. The feasibility of the approach is demonstrated through simulation and Monte Carlo runs.en_US
dc.language.isoen_USen_US
dc.publisherGeorgia Institute of Technologyen_US
dc.subjectControl signalsen_US
dc.subjectFeedbacken_US
dc.subjectFeedforward-feedback controlen_US
dc.subjectFlight management systemsen_US
dc.subjectNavigation performanceen_US
dc.subjectNominal controlen_US
dc.subjectNominal trajectoryen_US
dc.subjectOptimal controlen_US
dc.titleOptimal Trajectory Generation for Next Generation Flight Management Systemsen_US
dc.typePre-printen_US
dc.typeProceedingsen_US
dc.contributor.corporatenameGeorgia Institute of Technology. School of Electrical and Computer Engineeringen_US
dc.contributor.corporatenameGeorgia Institute of Technology. Center for Robotics and Intelligent Machinesen_US
dc.contributor.corporatenameRockwell Collinsen_US
dc.publisher.originalInstitute of Electrical and Electronics Engineers
dc.identifier.doi10.1109/DASC.2013.6712566
dc.embargo.termsnullen_US


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