Please use this identifier to cite or link to this item:
http://hdl.handle.net/10397/87763
DC Field | Value | Language |
---|---|---|
dc.contributor | Department of Industrial and Systems Engineering | - |
dc.creator | Ding, L | - |
dc.creator | Li, YM | - |
dc.date.accessioned | 2020-08-19T06:26:50Z | - |
dc.date.available | 2020-08-19T06:26:50Z | - |
dc.identifier.issn | 1756-8293 | - |
dc.identifier.uri | http://hdl.handle.net/10397/87763 | - |
dc.language.iso | en | en_US |
dc.publisher | SAGE Publications | en_US |
dc.rights | © The Author(s) 2020 | en_US |
dc.rights | Creative Commons Non Commercial CC BY-NC: This article is distributed under the terms of the Creative Commons Attribution-NonCommercial 4.0 License (https://creativecommons.org/licenses/by-nc/4.0/) which permits non-commercial use, reproduction and distributionof the work without further permission provided the original work is attributed as specified on the SAGE and Open Access pages (https://us.sagepub.com/en-us/nam/open-access-at-sage). | en_US |
dc.rights | The following publication Ding, L. , & Li, Y. M. (2020). Optimal attitude tracking control for an unmanned aerial quadrotor under lumped disturbances. International Journal of Micro Air Vehicles, 12, 1-14 is available at https://dx.doi.org/10.1177/1756829320923563 | en_US |
dc.subject | Quadrotor | en_US |
dc.subject | Attitude tracking control | en_US |
dc.subject | Terminal sliding mode | en_US |
dc.subject | Linear extended state observer | en_US |
dc.subject | Fruit fly optimization algorithm | en_US |
dc.title | Optimal attitude tracking control for an unmanned aerial quadrotor under lumped disturbances | en_US |
dc.type | Journal/Magazine Article | en_US |
dc.identifier.spage | 1 | - |
dc.identifier.epage | 14 | - |
dc.identifier.volume | 12 | - |
dc.identifier.doi | 10.1177/1756829320923563 | - |
dcterms.abstract | The robust control problem in attitude tracking of an unmanned aerial vehicle quadrotor is a challenging task due to strong parametric uncertainties, large nonlinearities and high couplings in flight dynamics. In this paper, a continuous nonsingular fast terminal sliding mode controller based on linear extended state observer is proposed for attitude tracking control of a quadrotor under lumped disturbances. The proposed control method requires no prior knowledge of the attitude dynamics. It can ensure rapid convergence rate and high tracking precision due to terminal sliding mode surface and fast reaching law. The controller uses the linear extended state observer to reject the influence of both parametric uncertainties and external disturbances. Meanwhile, the nonsingular fast terminal sliding mode control strategy is designed to ensure the state variables to slide to desired points in finite time. To enhance the control performance, a self-adaptive fruit fly optimization algorithm is applied to parameters tuning of the proposed controller. The effectiveness of the proposed control approach is illustrated through numerical simulations and experimental verification. | - |
dcterms.accessRights | open access | en_US |
dcterms.bibliographicCitation | International journal of micro air vehicles, 2020, v. 12, p. 1-14 | - |
dcterms.isPartOf | International journal of micro air vehicles | - |
dcterms.issued | 2020 | - |
dc.identifier.isi | WOS:000540008700001 | - |
dc.identifier.scopus | 2-s2.0-85085974332 | - |
dc.identifier.eissn | 1756-8307 | - |
dc.description.validate | 202008 bcrc | - |
dc.description.oa | Version of Record | en_US |
dc.identifier.FolderNumber | OA_Scopus/WOS | en_US |
dc.description.pubStatus | Published | en_US |
dc.description.oaCategory | CC | en_US |
Appears in Collections: | Journal/Magazine Article |
Files in This Item:
File | Description | Size | Format | |
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Ding_Unmanned_Aerial_Quadrotor.pdf | 1.17 MB | Adobe PDF | View/Open |
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