Trajectory tracking control method based on adaptive super-twisting sliding mode
Aiming at the problem of trajectory tracking control in the process of missile network formation flying, based on the optimal nominal trajectory obtained by solving the two-point boundary value problem, combined with the anti-jamming characteristics of the sliding mode controller, a trajectory track...
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Format: | Article |
Language: | zho |
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EDP Sciences
2022-10-01
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Series: | Xibei Gongye Daxue Xuebao |
Subjects: | |
Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2022/05/jnwpu2022405p1109/jnwpu2022405p1109.html |
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author | QI Zhaohui ZHANG Jin WANG Yuanzhuo WANG Jia XU Mengrong ZHANG Cheng |
author_facet | QI Zhaohui ZHANG Jin WANG Yuanzhuo WANG Jia XU Mengrong ZHANG Cheng |
author_sort | QI Zhaohui |
collection | DOAJ |
description | Aiming at the problem of trajectory tracking control in the process of missile network formation flying, based on the optimal nominal trajectory obtained by solving the two-point boundary value problem, combined with the anti-jamming characteristics of the sliding mode controller, a trajectory tracking control method based on the adaptive super-twisting sliding mode is proposed. First, on the basis of the terminal guidance section model, the two-point boundary value problem is solved through the idea of nonlinear programming to obtain the optimal nominal trajectory; Secondly, the tracking controller based on state deviation is designed in combination with the adaptive super-twisting sliding mode algorithm; Finally, the LQR trajectory tracking control method is introduced as a comparison method, and the effectiveness and feasibility of the sliding mode trajectory tracking method in the presence of initial state errors are verified by simulations, and the Monte Carlo simulation shows that the proposed method has good trajectory tracking control effect in the presence of different initial state errors. |
first_indexed | 2024-03-11T13:56:44Z |
format | Article |
id | doaj.art-fbf65e4b0d0544f796e8dc344d5f4017 |
institution | Directory Open Access Journal |
issn | 1000-2758 2609-7125 |
language | zho |
last_indexed | 2024-03-11T13:56:44Z |
publishDate | 2022-10-01 |
publisher | EDP Sciences |
record_format | Article |
series | Xibei Gongye Daxue Xuebao |
spelling | doaj.art-fbf65e4b0d0544f796e8dc344d5f40172023-11-02T06:57:52ZzhoEDP SciencesXibei Gongye Daxue Xuebao1000-27582609-71252022-10-014051109111510.1051/jnwpu/20224051109jnwpu2022405p1109Trajectory tracking control method based on adaptive super-twisting sliding modeQI Zhaohui0ZHANG Jin1WANG Yuanzhuo2WANG Jia3XU Mengrong4ZHANG Cheng5The Institute of Effectiveness Evaluation of Flying VehicleSchool of Astronautics, Northwestern Polytechnical UniversitySchool of Astronautics, Northwestern Polytechnical UniversityThe Institute of Effectiveness Evaluation of Flying VehicleThe Institute of Effectiveness Evaluation of Flying VehicleSchool of Automation, Xi'an University of Posts and TelecommunicationsAiming at the problem of trajectory tracking control in the process of missile network formation flying, based on the optimal nominal trajectory obtained by solving the two-point boundary value problem, combined with the anti-jamming characteristics of the sliding mode controller, a trajectory tracking control method based on the adaptive super-twisting sliding mode is proposed. First, on the basis of the terminal guidance section model, the two-point boundary value problem is solved through the idea of nonlinear programming to obtain the optimal nominal trajectory; Secondly, the tracking controller based on state deviation is designed in combination with the adaptive super-twisting sliding mode algorithm; Finally, the LQR trajectory tracking control method is introduced as a comparison method, and the effectiveness and feasibility of the sliding mode trajectory tracking method in the presence of initial state errors are verified by simulations, and the Monte Carlo simulation shows that the proposed method has good trajectory tracking control effect in the presence of different initial state errors.https://www.jnwpu.org/articles/jnwpu/full_html/2022/05/jnwpu2022405p1109/jnwpu2022405p1109.htmltrajectory trackingadaptive super-twisting sliding mode controlmonte carlo |
spellingShingle | QI Zhaohui ZHANG Jin WANG Yuanzhuo WANG Jia XU Mengrong ZHANG Cheng Trajectory tracking control method based on adaptive super-twisting sliding mode Xibei Gongye Daxue Xuebao trajectory tracking adaptive super-twisting sliding mode control monte carlo |
title | Trajectory tracking control method based on adaptive super-twisting sliding mode |
title_full | Trajectory tracking control method based on adaptive super-twisting sliding mode |
title_fullStr | Trajectory tracking control method based on adaptive super-twisting sliding mode |
title_full_unstemmed | Trajectory tracking control method based on adaptive super-twisting sliding mode |
title_short | Trajectory tracking control method based on adaptive super-twisting sliding mode |
title_sort | trajectory tracking control method based on adaptive super twisting sliding mode |
topic | trajectory tracking adaptive super-twisting sliding mode control monte carlo |
url | https://www.jnwpu.org/articles/jnwpu/full_html/2022/05/jnwpu2022405p1109/jnwpu2022405p1109.html |
work_keys_str_mv | AT qizhaohui trajectorytrackingcontrolmethodbasedonadaptivesupertwistingslidingmode AT zhangjin trajectorytrackingcontrolmethodbasedonadaptivesupertwistingslidingmode AT wangyuanzhuo trajectorytrackingcontrolmethodbasedonadaptivesupertwistingslidingmode AT wangjia trajectorytrackingcontrolmethodbasedonadaptivesupertwistingslidingmode AT xumengrong trajectorytrackingcontrolmethodbasedonadaptivesupertwistingslidingmode AT zhangcheng trajectorytrackingcontrolmethodbasedonadaptivesupertwistingslidingmode |