dc.contributor.author | Μαράντος, Παναγιώτης | el |
dc.contributor.author | Marantos, Panos | en |
dc.date.accessioned | 2015-12-23T08:49:57Z | |
dc.date.available | 2015-12-23T08:49:57Z | |
dc.date.issued | 2015-12-23 | |
dc.identifier.uri | https://dspace.lib.ntua.gr/xmlui/handle/123456789/41805 | |
dc.identifier.uri | http://dx.doi.org/10.26240/heal.ntua.1998 | |
dc.rights | Αναφορά Δημιουργού-Όχι Παράγωγα Έργα 3.0 Ελλάδα | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nd/3.0/gr/ | * |
dc.subject | Μη επανδρωμένα εναέρια οχήματα | el |
dc.subject | Μη γραμμικός έλεγχος | el |
dc.subject | Συστήματα πλοήγησης | el |
dc.subject | Οπτική ανατροφοδότηση | el |
dc.subject | Εύρωστος έλεγχος | el |
dc.subject | Unmanned Aerial Vehicles | en |
dc.subject | Navigation systems | en |
dc.subject | Nonlinear control | en |
dc.subject | Visual Servoing | en |
dc.subject | Robust Control | en |
dc.title | Dynamic Maneuvers for a Robotic Helicopter via Visual Feedback | en |
dc.title | Επιδέξιοι Ελιγμοί Ρομποτικού Ελικοπτέρου με Χρήση Οπτικής Ανατροφοδότησης | el |
dc.contributor.department | Τομέας Μηχανολογικών Κατασκευών & Αυτομάτου Ελέγχου | el |
heal.type | doctoralThesis | |
heal.classification | Ρομποτική | el |
heal.language | el | |
heal.language | en | |
heal.access | free | |
heal.recordProvider | ntua | el |
heal.publicationDate | 2015-11-03 | |
heal.abstract | In this Dissertation we address the problem of designing a reliable aerial embedded system dedicated for autonomous unmanned helicopters. We mainly focus on navigation and motion control systems using visual feedback. In the same vein, model-free control approaches are adopted in order to succeed robust autonomous flights in dynamic environments, exploiting a wide-range of helicopters’ flight envelope as well. First, we design and prototype low-cost onboard and ground systems -both hardware and software- in order to i) convert a remotely operated small-scale helicopter into an autonomous robotic platform and ii) construct a user-friendly ground station. Additionally, a non-linear mathematical model of flybarless helicopters is derived which will be used both in the navigation and control design, as well as in a realistic simulation framework. Regarding the navigation system, we propose a real-time, high-performance observer based on low-complex, robust and adaptive algorithms. Particularly, we use the complementary notion, fusing low-cost navigation sensors along with visual feedback, to extract the helicopter state vector. An adaptation scheme is also provided to allow unhindered operation of the filter to erroneous inputs introduced not only by the characteristics of low-cost sensors (i.e., biases, operation ranges, etc), but also by the high dynamics of aggressive maneuvers. Subsequently, we design robust model-based and model-free control schemes to stabilize the helicopter in various flight conditions, even under the presence of external disturbances, such as wind gusts or ground effect phenomena, which mainly affect the landing procedure. Finally, extensive autonomous flights are conducted with the Autonomous CSL Helicopter, called “mini-Daedalus”, demonstrating the efficacy of the proposed embedded system in highly demanding conditions and validating our design, navigation and control methods. | en |
heal.advisorName | Κυριακόπουλος, Κωνσταντίνος | el |
heal.committeeMemberName | Κυριακόπουλος, Κωνσταντίνος | el |
heal.committeeMemberName | Παπαδόπουλος, Ευάγγελος | el |
heal.committeeMemberName | Κρικέλης, Νικόλαος | el |
heal.committeeMemberName | Βουτσινάς, Σπυρίδων | el |
heal.committeeMemberName | Αντωνιάδης, Ιωάννης | el |
heal.committeeMemberName | Παπαλάμπρου, Γεώργιος | el |
heal.committeeMemberName | Τζές, Αντώνιος | el |
heal.academicPublisher | Σχολή Μηχανολόγων Μηχανικών | el |
heal.academicPublisherID | ntua | |
heal.numberOfPages | 359 | |
heal.fullTextAvailability | true |
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