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...

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Format: Article
Language:zho
Published: EDP Sciences 2018-04-01
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
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publishDate 2018-04-01
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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