VGU RESEARCH REPOSITORY
Please use this identifier to cite or link to this item:
https://epub.vgu.edu.vn/handle/dlibvgu/81
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Tran Trung Thanh | en_US |
dc.contributor.author | Oscar R Gonzalez | en_US |
dc.date.accessioned | 2020-03-12T16:54:40Z | - |
dc.date.available | 2020-03-12T16:54:40Z | - |
dc.date.issued | 2019 | - |
dc.identifier.citation | https://doi.org/10.1177/0959651819860294 | en_US |
dc.identifier.uri | http://epub.vgu.edu.vn/handle/dlibvgu/81 | - |
dc.description.abstract | This article investigates a backstepping-based control method for aircraft roll dynamics. The research starts with a formulation of backstepping control law for a general class of a strict-feedback form of nonlinear dynamic systems. The backstepping control law is formulated by introducing a normal tracking error. Then, control and virtual control inputs are selected by addressing each layer of the design process with a chosen corresponding control Lyapunov function. The parameter assignment in each design layer is selected to ensure the stability of the entire system. Next, a backstepping-based control algorithm with online-gain schedule or variable gains is provided for the standard strict-feedback system. In order to validate the proposed method, application of roll dynamics of aircraft is implemented. Dynamic equations of free-to-roll aircraft model is restructured in a standard strict-feedback model for formulating the backstepping control. Then, a backstepping control–based control strategy is provided for aircraft free-to-roll dynamics. Indoor experimental and simulation studies of roll angle control for the L-59 free-to-roll aircraft model at NASA Langley Research Center are implemented to verify and validate the proposed approach. | en_US |
dc.language.iso | en | en_US |
dc.publisher | SAGE | en_US |
dc.relation.ispartofseries | Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering (First and Cor); | - |
dc.subject | Nonlinear control | en_US |
dc.subject | Backstepping control | en_US |
dc.subject | Flight control | en_US |
dc.title | Backstepping-based control methodology for aircraft roll dynamics | en_US |
dc.type | Article | en_US |
dc.relation.journaltype | SCIE Q3 | en_US |
item.grantfulltext | none | - |
item.fulltext | No Fulltext | - |
item.languageiso639-1 | other | - |
Appears in Collections: | ARTICLE/BOOK PUBLICATION |
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