通过多目标配置优化设计提高人体离心机系统的性能

IF 2.1 3区 工程技术 Q2 ENGINEERING, AEROSPACE
Asher Winter, N. Mohajer, D. Nahavandi, Shady Mohamed
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引用次数: 0

摘要

人体离心系统(hcs)是提高机组人员加速度和空间定向障碍(SD)容忍度的有效训练工具。虽然高性能的hcs是可用的,但它们的结构和性能尚未得到充分优化,以有效地重建使用飞机战斗演习(ACMs)产生的g向量。为了实现这种改进,应该深入研究结构设计与HCS性能之间的关系。本工作提出了一个框架,以确定一个主动四自由度(DoF) HCS的最佳配置设计。利用逆运动学和动力学方法建立了构型设计参数与客观准则之间的关系。然后,利用多目标进化优化算法确定最佳臂长和座位位置,以最小化科里奥利效应、相对加速度比和成本。工作结果表明,应用的优化步骤可以显著有助于(1)有效地复制飞机运动,(2)最小化HCS运动期间产生的有害影响,以及(3)降低系统的总体成本。应用的方法可以适应具有不同结构和自由度的hcs。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Performance Improvement of Human Centrifuge Systems through Multi-Objective Configurational Design Optimisation
Human Centrifuge Systems (HCSs) are an effective training tool to improve the G-acceleration and Spatial Disorientation (SD) tolerance of aircrew. Though highly capable HCSs are available, their structure and performance are yet to be fully optimised to efficiently recreate the G-vectors produced using Aircraft Combat Manoeuvres (ACMs). To achieve this improvement, the relationship between configurational design and HCS performance should be profoundly investigated. This work proposes a framework for identifying the optimal configurational design of an active four Degree-of-Freedom (DoF) HCS. The relationship between configurational design parameters and objective criteria is established using inverse kinematics and dynamics. Then, a multi-objective evolutionary optimiser is used to identify the optimum arm length and seat position, minimising the Coriolis effect, relative acceleration ratio, and cost. The results of the work show that the applied optimisation step can significantly contribute to (1) efficiently replicating the aircraft motion, (2) minimising the detrimental effects generated during HCS motion, and (3) reducing the overall cost of the system. The applied methodology can be adapted to HCSs with different structures and DoFs.
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来源期刊
Aerospace
Aerospace ENGINEERING, AEROSPACE-
CiteScore
3.40
自引率
23.10%
发文量
661
审稿时长
6 weeks
期刊介绍: Aerospace is a multidisciplinary science inviting submissions on, but not limited to, the following subject areas: aerodynamics computational fluid dynamics fluid-structure interaction flight mechanics plasmas research instrumentation test facilities environment material science structural analysis thermophysics and heat transfer thermal-structure interaction aeroacoustics optics electromagnetism and radar propulsion power generation and conversion fuels and propellants combustion multidisciplinary design optimization software engineering data analysis signal and image processing artificial intelligence aerospace vehicles'' operation, control and maintenance risk and reliability human factors human-automation interaction airline operations and management air traffic management airport design meteorology space exploration multi-physics interaction.
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