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基于预定义时间的直接升力着舰增量控制

李煜 陈通文 王志刚 温志湧 刘小雄

航空学报2025,Vol.46Issue(13):84-100,17.
航空学报2025,Vol.46Issue(13):84-100,17.DOI:10.7527/S1000-6893.2024.31163

基于预定义时间的直接升力着舰增量控制

Incremental control of direct lift landing based on predefined-time theory

李煜 1陈通文 2王志刚 3温志湧 4刘小雄2

作者信息

  • 1. 香港理工大学 航空及民航工程学系,香港 999077||西北工业大学 自动化学院,西安 710072
  • 2. 西北工业大学 自动化学院,西安 710072
  • 3. 南京航空航天大学 自动化学院,南京 210016||中国航空工业集团 沈阳飞机设计研究所,沈阳 110035
  • 4. 香港理工大学 航空及民航工程学系,香港 999077
  • 折叠

摘要

Abstract

To address the disturbance of carrier wake and deck motion to carrier-based aircraft,this paper combines direct lift technology and incremental nonlinear control based on the predefined-time theory to improve the landing ac-curacy of carrier-based aircraft.Firstly,the full-state nonlinear dynamic equations of the aircraft are established,and the mechanisms and advantages of the direct lift control technology are analyzed.Secondly,an incremental control method based on the predefined-time theory is proposed,and an automatic landing controller for the carrier-based air-craft,consisting of the attitude stabilization loop,altitude control loop,and approach power compensation system,is designed based on this method.The designed automatic landing controller ensures that the tracking error of the carrier-based aircraft state converges to an adjustable bounded range within a predefined time,even under the influence of disturbances,thus enhancing its ability to rapidly track landing trajectory commands and deck movements.Moreover,this controller utilizes its robustness to reduce the impact of the carrier wake on the carrier-based aircraft.Subse-quently,the predefined-time stability of the automatic landing closed-loop control system is rigorously proven under the Lyapunov stability theory.Finally,a series of real-time simulations verifies the effectiveness and superiority of the de-signed automatic landing controller.

关键词

直接升力着舰/预定义时间控制/增量非线性控制/舰尾流抑制/非线性跟踪微分器

Key words

direct lift-based carrier-based aircraft landing/predefined-time control/incremental nonlinear control/air wake suppression/nonlinear tracking differentiator

分类

航空航天

引用本文复制引用

李煜,陈通文,王志刚,温志湧,刘小雄..基于预定义时间的直接升力着舰增量控制[J].航空学报,2025,46(13):84-100,17.

基金项目

国家自然科学基金(62073266) (62073266)

航空科学基金(201905053003) National Natural Science Foundation of China(62073266) (201905053003)

Aeronautical Science Foundation of China(201905053003) (201905053003)

航空学报

OA北大核心

1000-6893

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