Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/116456
DC FieldValueLanguage
dc.contributorDepartment of Aeronautical and Aviation Engineeringen_US
dc.contributorResearch Centre for Low Altitude Economyen_US
dc.creatorChan, YYen_US
dc.creatorShu, Yen_US
dc.creatorChen, WHen_US
dc.creatorNg, KKen_US
dc.date.accessioned2025-12-30T07:21:19Z-
dc.date.available2025-12-30T07:21:19Z-
dc.identifier.issn1270-9638en_US
dc.identifier.urihttp://hdl.handle.net/10397/116456-
dc.language.isoenen_US
dc.publisherElsevier Massonen_US
dc.subjectCable-suspended payload quadcoptersen_US
dc.subjectMotion planningen_US
dc.subject3D curve frameen_US
dc.titleTime-optimal motion planning of cable-suspended payload quadcopters using spatial reformulationen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.volume169en_US
dc.identifier.doi10.1016/j.ast.2025.111460en_US
dcterms.abstractCable-suspended payload quadcopters (CSPQ) have gained significant attention due to their mechanical simplicity and agility for various applications. However, the presence of a slung payload introduces complex dynamics, making the system highly underactuated and challenging to control. An accurate and intuitive representation of the safety region is also critical for collision avoidance as the operating environment is always complex and cluttered. This paper proposes a unified hierarchical framework for time-optimal motion planning and trajectory tracking of CSPQ systems, built upon a novel spatial reformulation method leveraging the Gravity-Normal (GN) frame. As an alternative to conventional reformulation approaches, this method transforms the system positions into path-parametric coordinates with clear physical interpretation and no singularities, thereby simplifying the representation of spatial constraints. The hierarchical framework comprises an offline module for global time-optimal trajectory generation using the direct multiple shooting method and an online module for real-time trajectory tracking through nonlinear model predictive control (NMPC). Simulation experiments demonstrated the effectiveness of the proposed framework in achieving time-optimal motion while suppressing payload oscillations within acceptable limits.en_US
dcterms.accessRightsembargoed accessen_US
dcterms.bibliographicCitationAerospace science and technology, Feb. 2026, v. 169, 111460en_US
dcterms.isPartOfAerospace science and technologyen_US
dcterms.issued2026-02-
dc.identifier.eissn1626-3219en_US
dc.identifier.artn111460en_US
dc.description.validate202512 bcwhen_US
dc.description.oaNot applicableen_US
dc.identifier.FolderNumberG000489b/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), the National Natural Science Foundation of China (Grant number: 72301229), and the Research Institute of Sustainable Urban Development (BBG5).en_US
dc.description.pubStatusPublisheden_US
dc.date.embargo2028-02-29en_US
dc.description.oaCategoryGreen (AAM)en_US
Appears in Collections:Journal/Magazine Article
Open Access Information
Status embargoed access
Embargo End Date 2028-02-29
Access
View full-text via PolyU eLinks SFX Query
Show simple item record

Google ScholarTM

Check

Altmetric


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.