起落架
控制理论(社会学)
减震器
工程类
控制器(灌溉)
模糊逻辑
稳健性(进化)
振动
休克(循环)
模糊控制系统
控制工程
计算机科学
航空航天工程
声学
控制(管理)
物理
医学
农学
生物化学
化学
人工智能
基因
内科学
生物
作者
Ahmet Enes Arık,Boğaç Bilgiç
出处
期刊:Aircraft Engineering and Aerospace Technology
[Emerald (MCB UP)]
日期:2022-07-29
卷期号:95 (2): 284-291
被引量:1
标识
DOI:10.1108/aeat-01-2022-0028
摘要
Purpose The purpose of this paper is to control a landing gear system with an oleo-pneumatic shock absorber with the fuzzy controller. Design/methodology/approach The landing gear system with an oleo-pneumatic shock absorber is modeled mathematically. A fuzzy controller is designed for reducing aircraft vibrations. Stroke velocity and main mass velocity parameters were used to decide variable gas pressure with the fuzzy controller. Findings The fuzzy controller, designed according to stroke velocity and main mass velocity, reduces aircraft vibrations by the landing impacts. The controller can provide strong robustness because it shows similar good performance for different descent speeds. Research limitations/implications This study was carried out through simulations in a computer environment and has not been experimentally tested in a real environment. In addition, signal and measurement delays are not taken into account. In future models, the effects of these signal delays can be added, and the controller can be tested on a real model. Originality/value In this study, to the best of the authors’ knowledge, for the first time, the gas pressure for the landing gear system using an oleo-pneumatic shock absorber was controlled by a fuzzy controller that adjusts the stroke velocity and the main mass velocity. Although the oleo-pneumatic shock absorber model contains high nonlinearities, the designed fuzzy controller gave successful results as robust.
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