Attitude Stabilization and Trajectory Tracking Control Strategy for Civil UAV
To remove the funitional payload variation, the attitude oscillation and trajectory tracking error of civil UAV in complex environment, a combined inner and outer control strategy for the civil UAV is designed based on the interval system control theory and dynamic tracking error minimization princi...
Format: | Article |
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Language: | zho |
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EDP Sciences
2018-04-01
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Series: | Xibei Gongye Daxue Xuebao |
Subjects: | |
Online Access: | https://www.jnwpu.org/articles/jnwpu/pdf/2018/02/jnwpu2018362p382.pdf |
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collection | DOAJ |
description | To remove the funitional payload variation, the attitude oscillation and trajectory tracking error of civil UAV in complex environment, a combined inner and outer control strategy for the civil UAV is designed based on the interval system control theory and dynamic tracking error minimization principle, which can guarantee the attitude stabilization in inner loop and the heading tracking in outer loop, thus solving the control effect deterioration and trajectory error drawback of the existing UAV with large scale model variation. The simulation results show that, the proposed combined control strategy can keep flight state's stabilization and effective trajectory tracking with good closed-loop robustness. This study is useful to develop effective and automatic civil UAV system's flight control strategy. |
first_indexed | 2024-03-11T20:36:29Z |
format | Article |
id | doaj.art-95cc505dd1fd4cfca7b1cafc900f1dcd |
institution | Directory Open Access Journal |
issn | 1000-2758 2609-7125 |
language | zho |
last_indexed | 2024-03-11T20:36:29Z |
publishDate | 2018-04-01 |
publisher | EDP Sciences |
record_format | Article |
series | Xibei Gongye Daxue Xuebao |
spelling | doaj.art-95cc505dd1fd4cfca7b1cafc900f1dcd2023-10-02T06:29:09ZzhoEDP SciencesXibei Gongye Daxue Xuebao1000-27582609-71252018-04-0136238238710.1051/jnwpu/20183620382jnwpu2018362p382Attitude Stabilization and Trajectory Tracking Control Strategy for Civil UAV012School of Flight TechnologySchool of Flight TechnologySchool of Flight TechnologyTo remove the funitional payload variation, the attitude oscillation and trajectory tracking error of civil UAV in complex environment, a combined inner and outer control strategy for the civil UAV is designed based on the interval system control theory and dynamic tracking error minimization principle, which can guarantee the attitude stabilization in inner loop and the heading tracking in outer loop, thus solving the control effect deterioration and trajectory error drawback of the existing UAV with large scale model variation. The simulation results show that, the proposed combined control strategy can keep flight state's stabilization and effective trajectory tracking with good closed-loop robustness. This study is useful to develop effective and automatic civil UAV system's flight control strategy.https://www.jnwpu.org/articles/jnwpu/pdf/2018/02/jnwpu2018362p382.pdfcivil uavflight attitudeinterval systemstability controltrajectory trackingcontrolunmanned aerial vehicles |
spellingShingle | Attitude Stabilization and Trajectory Tracking Control Strategy for Civil UAV Xibei Gongye Daxue Xuebao civil uav flight attitude interval system stability control trajectory tracking control unmanned aerial vehicles |
title | Attitude Stabilization and Trajectory Tracking Control Strategy for Civil UAV |
title_full | Attitude Stabilization and Trajectory Tracking Control Strategy for Civil UAV |
title_fullStr | Attitude Stabilization and Trajectory Tracking Control Strategy for Civil UAV |
title_full_unstemmed | Attitude Stabilization and Trajectory Tracking Control Strategy for Civil UAV |
title_short | Attitude Stabilization and Trajectory Tracking Control Strategy for Civil UAV |
title_sort | attitude stabilization and trajectory tracking control strategy for civil uav |
topic | civil uav flight attitude interval system stability control trajectory tracking control unmanned aerial vehicles |
url | https://www.jnwpu.org/articles/jnwpu/pdf/2018/02/jnwpu2018362p382.pdf |