环境干扰下航母自动着陆的全局快速终端滑动模式控制

IF 1.2 4区 工程技术 Q3 ENGINEERING, AEROSPACE Aircraft Engineering and Aerospace Technology Pub Date : 2024-03-29 DOI:10.1108/aeat-10-2023-0273
Zhuoer Yao, Zi Kan, Daochun Li, Haoyuan Shao, Jinwu Xiang
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引用次数: 0

摘要

目的 本文旨在解决存在环境干扰的航母自动着陆这一难题。首先,建立了航母自动着陆系统的框架,包括飞行滑行路径模型、制导模型、进近功率补偿系统和飞行控制器模型。随后,介绍了航母甲板运动模型和航母气浮模型,以模拟环境干扰。然后,提供了 GFTSMC 的详细设计步骤。通过莱普诺夫定理和拉萨尔不变性原理证明了控制器的稳定性分析。此外,还进行了到达时间分析,证明控制器具有固定时间收敛能力。仿真结果表明,所提出的方法能保证有限的收敛时间,并能在各种条件下保证航母安全着陆。原创性/价值本文提出的 GFTSMC 方法能在环境干扰下实现精确、安全的载机着陆,对改进 ACLS 控制器设计具有重要的参考意义。
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Global fast terminal sliding mode control for automatic carrier landing with environmental disturbances

Purpose

The purpose of this paper is to solve the challenging problem of automatic carrier landing with the presence of environmental disturbances. Therefore, a global fast terminal sliding mode control (GFTSMC) method is proposed for automatic carrier landing system (ACLS) to achieve safe carrier landing control.

Design/methodology/approach

First, the framework of ACLS is established, which includes flight glide path model, guidance model, approach power compensation system and flight controller model. Subsequently, the carrier deck motion model and carrier air-wake model are presented to simulate the environmental disturbances. Then, the detailed design steps of GFTSMC are provided. The stability analysis of the controller is proved by Lyapunov theorems and LaSalle’s invariance principle. Furthermore, the arrival time analysis is carried out, which proves the controller has fixed time convergence ability.

Findings

The numerical simulations are conducted. The simulation results reveal that the proposed method can guarantee a finite convergence time and safe carrier landing under various conditions. And the superiority of the proposed method is further demonstrated by comparative simulations and Monte Carlo tests.

Originality/value

The GFTSMC method proposed in this paper can achieve precise and safe carrier landing with environmental disturbances, which has important referential significance to the improvement of ACLS controller designs.

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来源期刊
Aircraft Engineering and Aerospace Technology
Aircraft Engineering and Aerospace Technology 工程技术-工程:宇航
CiteScore
3.20
自引率
13.30%
发文量
168
审稿时长
8 months
期刊介绍: Aircraft Engineering and Aerospace Technology provides a broad coverage of the materials and techniques employed in the aircraft and aerospace industry. Its international perspectives allow readers to keep up to date with current thinking and developments in critical areas such as coping with increasingly overcrowded airways, the development of new materials, recent breakthroughs in navigation technology - and more.
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