Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/117428
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dc.contributorDepartment of Aeronautical and Aviation Engineering-
dc.creatorYang, P-
dc.creatorWen, W-
dc.creatorBai, S-
dc.creatorHu, J-
dc.date.accessioned2026-02-25T01:23:02Z-
dc.date.available2026-02-25T01:23:02Z-
dc.identifier.issn0018-9251-
dc.identifier.urihttp://hdl.handle.net/10397/117428-
dc.language.isoenen_US
dc.publisherInstitute of Electrical and Electronics Engineersen_US
dc.rights© 2025 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.en_US
dc.rightsThe following publication P. Yang, W. Wen, S. Bai and J. Hu, 'Online Dynamic Model Calibration for Reliable Control of Quadrotor Based on Factor Graph Optimization,' in IEEE Transactions on Aerospace and Electronic Systems, vol. 61, no. 5, pp. 11254-11266, Oct. 2025 is available at https://doi.org/10.1109/TAES.2025.3566347.en_US
dc.titleOnline dynamic model calibration for reliable control of quadrotor based on factor graph optimizationen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage11254-
dc.identifier.epage11266-
dc.identifier.volume61-
dc.identifier.issue5-
dc.identifier.doi10.1109/TAES.2025.3566347-
dcterms.abstractPrecise dynamic model calibration is essential in achieving reliable control of unmanned aerial vehicles (UAVs). However, the existing methods tend to use simplified dynamic models and cannot adapt to variations of the dynamic model. To fill this gap, this article explores an online dynamic model calibration (ODMC) method for the quadrotor based on factor graph optimization. First, the dynamic model is derived with more error terms, such as the center of gravity, aerodynamic drag, HVT disturbance, and viscous effect. Moreover, the IMU–body extrinsic parameters and the gravity vector are also identified online. Second, the pose is estimated based on the visual–inertial odometry together with the dynamic model parameters. The proposed method is validated using open-source and self-collected datasets. The evaluation demonstrates that the ODMC performs even better than the state-of-the-art data-driven methods in force and torque prediction when the maximum velocity is less than 9 m/s. Furthermore, the effectiveness of the proposed method is validated by applying the estimated model in the differential-flatness-based controller.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationIEEE transactions on aerospace and electronic systems, Oct. 2025, v. 61, no. 5, p. 11254-11266-
dcterms.isPartOfIEEE transactions on aerospace and electronic systems-
dcterms.issued2025-10-
dc.identifier.scopus2-s2.0-105004383888-
dc.identifier.eissn1557-9603-
dc.description.validate202602 bcjz-
dc.description.oaAccepted Manuscripten_US
dc.identifier.SubFormIDG001081/2026-02en_US
dc.description.fundingSourceRGCen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextThis work was supported in part by the innovation and technology fund under the project “Safety-Certified Multi-Source Fusion Positioning for Autonomous Vehicle in Complex Scenarios (ZPE8)” in part by the Germany/Hong Kong Joint Research Scheme under the project “Maximum Consensus Integration of GNSS and LiDAR (RADM)” in part by the Research Center of Deep Space Exploration (RC-DSE) under the project “Multi-Robot Collaborative Operations (BBDW)” in part by the PolyU Research Institute for Advanced Manufacturing (RIAM) under the project “Unmanned Aerial Vehicle Aided High Accuracy Addictive Manufacturing for Carbon Fiber Reinforced Thermoplastic Composites Material (CD8S).”en_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryGreen (AAM)en_US
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