Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/116329
DC FieldValueLanguage
dc.contributorDepartment of Aeronautical and Aviation Engineeringen_US
dc.creatorChan, YYen_US
dc.creatorNg, KKHen_US
dc.creatorWang, Ten_US
dc.creatorHon, KKen_US
dc.creatorLiu, CHen_US
dc.date.accessioned2025-12-16T06:41:11Z-
dc.date.available2025-12-16T06:41:11Z-
dc.identifier.issn0968-090Xen_US
dc.identifier.urihttp://hdl.handle.net/10397/116329-
dc.language.isoenen_US
dc.subjectAerial systemsen_US
dc.subjectCollision avoidanceen_US
dc.subjectMinimum-timeen_US
dc.subjectNonlinear model predictive controlen_US
dc.subjectSpatial reformulationen_US
dc.titleNear time-optimal trajectory optimisation for drones in last-mile delivery using spatial reformulation approachen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.volume171en_US
dc.identifier.doi10.1016/j.trc.2024.104986en_US
dcterms.abstractSeeking a computationally efficient and time-optimal trajectory for drones is crucial for saving time and energy costs, especially in the field of drone parcel delivery. Still, last-mile drone delivery is a challenge in urban environments, due to the existence of complex spatial constraints arising from high-rise buildings and the inherent non-linearity of the system dynamics. This paper presents a three-stage method to address the trajectory optimisation problem in a constrained environment. First, the kinematics and dynamics of the quadcopter are reformulated in terms of spatial coordinates, which enables the explicit evaluation of the progress of the path. Second, an efficient flight corridor generation algorithm is presented based on the transverse coordinates of the spatial reformulation. Third, the nonlinear model predictive control (NMPC)-based optimal control problem with obstacle avoidance is formulated for solving the time-optimal trajectory. Compared to the true time-optimal trajectory, the flight time of the near time-optimal trajectory is 3.10% longer than the true time-optimal trajectory, but with a 92.5% reduction in computation time. Numerical simulations based on an illustrative scenario as well as a real-world urban environment are conducted. Results demonstrate the effectiveness of the proposed method in generating near time-optimal trajectory but with a reduced computational burden.en_US
dcterms.accessRightsembargoed accessen_US
dcterms.bibliographicCitationTransportation research. Part C, Emerging technologies, Feb. 2025, v. 171, 104986en_US
dcterms.isPartOfTransportation research. Part C, Emerging technologiesen_US
dcterms.issued2025-02-
dc.identifier.scopus2-s2.0-85213865687-
dc.identifier.eissn1879-2359en_US
dc.identifier.artn104986en_US
dc.description.validate202512 bchyen_US
dc.description.oaNot applicableen_US
dc.identifier.SubFormIDG000489/2025-12-
dc.description.fundingSourceRGCen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextThe work described in this paper was supported by grants from the Research Grants Council, the Hong Kong Government (Grant No. PolyU15201423), Department of Aeronautical and Aviation Engineering , The Hong Kong Polytechnic University , Hong Kong SAR (RJ1D), Research Centre for Unmanned Autonomous Systems (CE1W) and the National Natural Science Foundation of China (Grant number: 72301229 ).en_US
dc.description.pubStatusPublisheden_US
dc.date.embargo2026-02-28en_US
dc.description.oaCategoryGreen (AAM)en_US
Appears in Collections:Journal/Magazine Article
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Embargo End Date 2026-02-28
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