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基于Super-Twisting滑模S面的无人机路径跟踪控制

张国兵 石上瑶 李佳成 常哲 陈鹏云

火力与指挥控制2024,Vol.49Issue(2):11-17,7.
火力与指挥控制2024,Vol.49Issue(2):11-17,7.DOI:10.3969/j.issn.1002-0640.2024.02.002

基于Super-Twisting滑模S面的无人机路径跟踪控制

Path Tracking Control of UAV Based on Super Twisting Sliding Mode S-Plane

张国兵 1石上瑶 1李佳成 1常哲 1陈鹏云1

作者信息

  • 1. 中北大学航空宇航学院,太原 030051
  • 折叠

摘要

Abstract

Aiming at the problems of low tracking accuracy and easy to be affected by external wind when small fixed wing UAV performs tasks,a path tracking controller based on the Super Twisting Sliding Mode S-Plane(STSM S-Plane)is designed,and the internal and external double loop control mode is adopted.The outer loop,namely the speed loop,adopts super twisting sliding mode control,and the inner loop,namely the attitude loop,adopts s-plane control.Considering that the der-ivation of S-plane control is easy to lead to integral explosion,the second-order differentiator is introduced,and the composition of the external wind is modeled and studied.The control performance of the designed algorithm is verified by spatial special curve.The simulation results show that the designed algorithm can achieve accurate tracking of the desired path of fixed wing UAV,and has good robustness and anti-interference performance.

关键词

固定翼无人机/Super-Twisting滑模/S面控制/风干扰

Key words

fixed wing UAV/super-twisting sliding mode/s-plane control/wind disturbance

分类

航空航天

引用本文复制引用

张国兵,石上瑶,李佳成,常哲,陈鹏云..基于Super-Twisting滑模S面的无人机路径跟踪控制[J].火力与指挥控制,2024,49(2):11-17,7.

基金项目

国家自然科学基金(51909245,62003314) (51909245,62003314)

山西省基础研究计划资助(201901D211244,202103021224187) (201901D211244,202103021224187)

中国航空科学基金资助项目(2019020U0002) (2019020U0002)

火力与指挥控制

OA北大核心CSTPCD

1002-0640

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