Adaptive control of unmanned aerial vehicles in atmospheric flight with reduced models
dc.contributor.author | Kahveci, N. E. | en |
dc.contributor.author | Ioannou, Petros A. | en |
dc.contributor.author | Mirmirani, M. D. | en |
dc.coverage.spatial | Los Angeles, CA | en |
dc.creator | Kahveci, N. E. | en |
dc.creator | Ioannou, Petros A. | en |
dc.creator | Mirmirani, M. D. | en |
dc.date.accessioned | 2019-12-02T10:35:51Z | |
dc.date.available | 2019-12-02T10:35:51Z | |
dc.date.issued | 2007 | |
dc.identifier.uri | http://gnosis.library.ucy.ac.cy/handle/7/57000 | |
dc.description.abstract | We propose an approximate implementation scheme for an adaptive linear quadratic control structure by employing a balanced truncation procedure in the loop prior to solving the associated Algebraic Riccati Equation (ARE). The control design combined with an adaptive law to compensate for uncertainties and possible changes in the dynamics is applied to the longitudinal model of an Unmanned Aerial Vehicle (UAV) in atmospheric flight. The tracking controllers based on the full and reduced order UAV models are constructed, and the resultant effect of the described model reduction on the flight performance of the vehicle is investigated through comparative simulations. Copyright © 2007 SAE International. | en |
dc.source | AeroTech Congress and Exhibition | en |
dc.source.uri | https://www.scopus.com/inward/record.uri?eid=2-s2.0-84877409567&doi=10.4271%2f2007-01-3899&partnerID=40&md5=46c371b493be6f93634200d0650358aa | |
dc.subject | Computer simulation | en |
dc.subject | Linear control systems | en |
dc.subject | Riccati equations | en |
dc.subject | Exhibitions | en |
dc.subject | Model reduction | en |
dc.subject | Reduced model | en |
dc.subject | Adaptive Control | en |
dc.subject | Control design | en |
dc.subject | Adaptive laws | en |
dc.subject | Flight simulators | en |
dc.subject | Unmanned aerial vehicles (UAV) | en |
dc.subject | Adaptive linear quadratic controls | en |
dc.subject | Algebraic Riccati equations | en |
dc.subject | Atmospheric flight | en |
dc.subject | Balanced truncation | en |
dc.subject | Comparative simulation | en |
dc.subject | Implementation scheme | en |
dc.subject | Reduced order | en |
dc.subject | Tracking controller | en |
dc.title | Adaptive control of unmanned aerial vehicles in atmospheric flight with reduced models | en |
dc.type | info:eu-repo/semantics/article | |
dc.identifier.doi | 10.4271/2007-01-3899 | |
dc.author.faculty | Σχολή Θετικών και Εφαρμοσμένων Επιστημών / Faculty of Pure and Applied Sciences | |
dc.author.department | Τμήμα Μαθηματικών και Στατιστικής / Department of Mathematics and Statistics | |
dc.type.uhtype | Article | en |
dc.description.notes | <p>Conference code: 90242 | en |
dc.description.notes | Cited By :1</p> | en |
dc.source.abbreviation | SAE Techni.Paper. | en |
dc.contributor.orcid | Ioannou, Petros A. [0000-0001-6981-0704] | |
dc.gnosis.orcid | 0000-0001-6981-0704 |
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