用于航母自动着陆的虚拟约束广义相对运动建模和控制参数优化器

IF 1.2 4区 工程技术 Q3 ENGINEERING, AEROSPACE Aircraft Engineering and Aerospace Technology Pub Date : 2024-04-05 DOI:10.1108/aeat-08-2023-0217
Yiwei Zhang, Daochun Li, Zi Kan, Zhuoer Yao, Jinwu Xiang
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引用次数: 0

摘要

目的 本文旨在提出一种新型控制方案,并提供一种控制参数优化器,以实现更好的航母自动着陆。航母着陆是一项极具挑战性的工作,因为其海况恶劣、精度要求高、飞机非线性和机动耦合。因此,航母自动着陆系统需要一种兼具高鲁棒性、快速性和准确性的控制方案。设计/方法/途径通过将期望状态和实际状态视为受约束的广义相对运动,构建了一个新颖的参考模型,作为一个虚拟的终端弹簧-阻尼系统。研究结果该控制参数优化器能高效、有效地获得经过良好调整的控制参数。原创性/价值与滑动模式控制和比例积分微分(PID)相比,所提出的控制方案具有更强的鲁棒性、准确性和快速性。同时,由于控制参数数量少、效率高,本文在飞行控制领域首次实现了所有控制参数的同步优化。
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Virtually constrained generalized relative motion modeling and a control parameter optimizer for automatic carrier landing

Purpose

This paper aims to propose a novel control scheme and offer a control parameter optimizer to achieve better automatic carrier landing. Carrier landing is a challenging work because of the severe sea conditions, high demand for accuracy and non-linearity and maneuvering coupling of the aircraft. Consequently, the automatic carrier landing system raises the need for a control scheme that combines high robustness, rapidity and accuracy. In addition, to exploit the capability of the proposed control scheme and alleviate the difficulty of manual parameter tuning, a control parameter optimizer is constructed.

Design/methodology/approach

A novel reference model is constructed by considering the desired state and the actual state as constrained generalized relative motion, which works as a virtual terminal spring-damper system. An improved particle swarm optimization algorithm with dynamic boundary adjustment and Pareto set analysis is introduced to optimize the control parameters.

Findings

The control parameter optimizer makes it efficient and effective to obtain well-tuned control parameters. Furthermore, the proposed control scheme with the optimized parameters can achieve safe carrier landings under various severe sea conditions.

Originality/value

The proposed control scheme shows stronger robustness, accuracy and rapidity than sliding-mode control and Proportion-integration-differentiation (PID). Also, the small number and efficiency of control parameters make this paper realize the first simultaneous optimization of all control parameters in the field of flight control.

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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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