A Moving Frame Trajectory Tracking Method of a Flying-Wing UAV Using the Differential Geometry

The problem of UAV trajectory tracking is a difficult issue for scholars and engineers, especially when the target curve is a complex curve in the three-dimensional space. In this paper, the coordinate frames during the tracking process are transformed to improve the tracking result. Firstly, the ba...

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Main Authors: Yi Zhu, Xin Chen, Chuntao Li
Format: Article
Language:English
Published: Hindawi Limited 2016-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2016/3406256
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spelling doaj-8c11f5c9058f410d8f6b06bed5081fc22020-11-25T01:08:51ZengHindawi LimitedInternational Journal of Aerospace Engineering1687-59661687-59742016-01-01201610.1155/2016/34062563406256A Moving Frame Trajectory Tracking Method of a Flying-Wing UAV Using the Differential GeometryYi Zhu0Xin Chen1Chuntao Li2College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCollege of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCollege of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaThe problem of UAV trajectory tracking is a difficult issue for scholars and engineers, especially when the target curve is a complex curve in the three-dimensional space. In this paper, the coordinate frames during the tracking process are transformed to improve the tracking result. Firstly, the basic concepts of the moving frame are given. Secondly the transfer principles of various moving frames are formulated and the Bishop frame is selected as a final choice for its flexibility. Thirdly, the detailed dynamic equations of the moving frame tracking method are formulated. In simulation, a moving frame of an elliptic cylinder helix is formulated precisely. Then, the devised tracking method on the basis of the dynamic equations is tested in a complete flight control system with 6 DOF nonlinear equations of the UAV. The simulation result shows a satisfactory trajectory tracking performance so that the effectiveness and efficiency of the devised tracking method is proved.http://dx.doi.org/10.1155/2016/3406256
collection DOAJ
language English
format Article
sources DOAJ
author Yi Zhu
Xin Chen
Chuntao Li
spellingShingle Yi Zhu
Xin Chen
Chuntao Li
A Moving Frame Trajectory Tracking Method of a Flying-Wing UAV Using the Differential Geometry
International Journal of Aerospace Engineering
author_facet Yi Zhu
Xin Chen
Chuntao Li
author_sort Yi Zhu
title A Moving Frame Trajectory Tracking Method of a Flying-Wing UAV Using the Differential Geometry
title_short A Moving Frame Trajectory Tracking Method of a Flying-Wing UAV Using the Differential Geometry
title_full A Moving Frame Trajectory Tracking Method of a Flying-Wing UAV Using the Differential Geometry
title_fullStr A Moving Frame Trajectory Tracking Method of a Flying-Wing UAV Using the Differential Geometry
title_full_unstemmed A Moving Frame Trajectory Tracking Method of a Flying-Wing UAV Using the Differential Geometry
title_sort moving frame trajectory tracking method of a flying-wing uav using the differential geometry
publisher Hindawi Limited
series International Journal of Aerospace Engineering
issn 1687-5966
1687-5974
publishDate 2016-01-01
description The problem of UAV trajectory tracking is a difficult issue for scholars and engineers, especially when the target curve is a complex curve in the three-dimensional space. In this paper, the coordinate frames during the tracking process are transformed to improve the tracking result. Firstly, the basic concepts of the moving frame are given. Secondly the transfer principles of various moving frames are formulated and the Bishop frame is selected as a final choice for its flexibility. Thirdly, the detailed dynamic equations of the moving frame tracking method are formulated. In simulation, a moving frame of an elliptic cylinder helix is formulated precisely. Then, the devised tracking method on the basis of the dynamic equations is tested in a complete flight control system with 6 DOF nonlinear equations of the UAV. The simulation result shows a satisfactory trajectory tracking performance so that the effectiveness and efficiency of the devised tracking method is proved.
url http://dx.doi.org/10.1155/2016/3406256
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AT yizhu movingframetrajectorytrackingmethodofaflyingwinguavusingthedifferentialgeometry
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