Optimal Fixed-Wing UAV Rendezvous Via LQR-Based Longitudinal Control
| dc.contributor.author | Buyukekiz, Kadir Bulathan | |
| dc.contributor.author | Ergezer, Halit | |
| dc.contributor.other | 06.08. Mekatronik Mühendisliği | |
| dc.contributor.other | 06. Mühendislik Fakültesi | |
| dc.contributor.other | 01. Çankaya Üniversitesi | |
| dc.date.accessioned | 2025-07-06T00:53:57Z | |
| dc.date.available | 2025-07-06T00:53:57Z | |
| dc.date.issued | 2025 | |
| dc.description.abstract | This paper proposes an optimal control-based rendezvous strategy for fixed-wing Unmanned Aerial Vehicles (UAVs) using a Linear Quadratic Regulator (LQR). The goal is precisely tracking a moving target while maintaining flight stability and avoiding predefined restricted areas. The controller optimally adjusts UAVs flight parameters to minimize trajectory errors and enhance robustness against environmental disturbances. A penalty-based method is integrated to prevent UAVs from entering restricted areas while ensuring smooth trajectory adaptation. The proposed approach has been tested in MATLAB simulations under multiple scenarios, demonstrating its effectiveness in achieving stable and efficient rendezvous maneuvers. The results confirm that LQR-based control and adaptive penalty mechanisms offer a practical solution for fixed-wing UAV operations in constrained environments. | en_US |
| dc.identifier.doi | 10.1109/ICUAS65942.2025.11007853 | |
| dc.identifier.isbn | 9798331513290 | |
| dc.identifier.isbn | 9798331513283 | |
| dc.identifier.issn | 2373-6720 | |
| dc.identifier.scopus | 2-s2.0-105007598107 | |
| dc.identifier.uri | https://doi.org/10.1109/ICUAS65942.2025.11007853 | |
| dc.language.iso | en | en_US |
| dc.publisher | IEEE | en_US |
| dc.relation.ispartof | 2025 International Conference on Unmanned Aircraft Systems-ICUAS-Annual -- MAY 14-17, 2025 -- Charlotte, NC | en_US |
| dc.relation.ispartofseries | International Conference on Unmanned Aircraft Systems | |
| dc.rights | info:eu-repo/semantics/closedAccess | en_US |
| dc.subject | LQR | en_US |
| dc.subject | Optimal Control | en_US |
| dc.subject | UAV | en_US |
| dc.subject | Fixed-Wing UAV | en_US |
| dc.subject | Rendezvous | en_US |
| dc.title | Optimal Fixed-Wing UAV Rendezvous Via LQR-Based Longitudinal Control | en_US |
| dc.title | Optimal Fixed-Wing UAV Rendezvous Via LQR-Based Longitudinal Control | |
| dc.type | Conference Object | en_US |
| dspace.entity.type | Publication | |
| gdc.author.institutional | Ergezer, Halit | |
| gdc.author.wosid | Ergezer, Halit/S-6502-2017 | |
| gdc.description.department | Çankaya University | en_US |
| gdc.description.departmenttemp | [Buyukekiz, Kadir Bulathan] Turkish Aerosp Ind, Flight & Miss Management Syst Dept, TR-06980 Ankara, Turkiye; [Ergezer, Halit] Cankaya Univ, Dept Mechatron Engn, Fac Engn, TR-06790 Ankara, Turkiye | en_US |
| gdc.description.endpage | 776 | en_US |
| gdc.description.publicationcategory | Konferans Öğesi - Uluslararası - Kurum Öğretim Elemanı | en_US |
| gdc.description.scopusquality | N/A | |
| gdc.description.startpage | 769 | en_US |
| gdc.description.woscitationindex | Conference Proceedings Citation Index - Science | |
| gdc.description.wosquality | N/A | |
| gdc.identifier.openalex | W4410770884 | |
| gdc.identifier.wos | WOS:001548686600102 | |
| gdc.openalex.fwci | 0.0 | |
| gdc.openalex.normalizedpercentile | 0.12 | |
| gdc.openalex.toppercent | TOP 10% | |
| gdc.opencitations.count | 0 | |
| gdc.plumx.mendeley | 2 | |
| gdc.plumx.scopuscites | 0 | |
| gdc.scopus.citedcount | 0 | |
| gdc.wos.citedcount | 0 | |
| relation.isAuthorOfPublication | e7c25403-d5d5-4ca7-b1c0-8e155d9a2310 | |
| relation.isAuthorOfPublication.latestForDiscovery | e7c25403-d5d5-4ca7-b1c0-8e155d9a2310 | |
| relation.isOrgUnitOfPublication | 5b0b2c59-0735-4593-b820-ff3847d58827 | |
| relation.isOrgUnitOfPublication | 43797d4e-4177-4b74-bd9b-38623b8aeefa | |
| relation.isOrgUnitOfPublication | 0b9123e4-4136-493b-9ffd-be856af2cdb1 | |
| relation.isOrgUnitOfPublication.latestForDiscovery | 5b0b2c59-0735-4593-b820-ff3847d58827 |