全尺寸飞蛾水翼控制系统试验台的研制

Sean Kebbell, J. Binns
{"title":"全尺寸飞蛾水翼控制系统试验台的研制","authors":"Sean Kebbell, J. Binns","doi":"10.2218/marine2021.6863","DOIUrl":null,"url":null,"abstract":". The design, construction and evaluation of a test platform to test the International Moth class in real world conditions was undertaken with the aim to investigate the effects of altering the value of the proportional control coefficient on flight modes to provide data for further numerical simulations. Through consultation with industry, technical experts and reviews of literature, a design was produced that allowed foils to be tested over a range of velocities, foil configurations and control systems that would be free to move in pitch and heave, however constrained in roll, yaw, sway and surge. The rig with the degrees of freedom can be seen below in Figure 1. Improvement of an existing electronic ride control system (ERCS) allowed the test moth to be able to fly at a range of depth to chord ratios along with the capability to change the respective flight modes with varying amplitudes. Ultimately, it was concluded that in a real-world environment the differences in drag between the range of values tested resulted in no serious measurable performance gains despite significant motion variations. However, it was apparent that small relationships formed and that it is essential for more research to be conducted in order to validate the data. The rig developed provides an easily accessible method for testing control algorithms in a real-world environment without the need for complex sailing configurations. The rig also allows cheap ways of tuning a system that is ripe for full on-water implementation.","PeriodicalId":367395,"journal":{"name":"The 9th Conference on Computational Methods in Marine Engineering (Marine 2021)","volume":"103 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-01-31","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Development of a Full Scale Moth Hydrofoil Control System Test Rig\",\"authors\":\"Sean Kebbell, J. Binns\",\"doi\":\"10.2218/marine2021.6863\",\"DOIUrl\":null,\"url\":null,\"abstract\":\". The design, construction and evaluation of a test platform to test the International Moth class in real world conditions was undertaken with the aim to investigate the effects of altering the value of the proportional control coefficient on flight modes to provide data for further numerical simulations. Through consultation with industry, technical experts and reviews of literature, a design was produced that allowed foils to be tested over a range of velocities, foil configurations and control systems that would be free to move in pitch and heave, however constrained in roll, yaw, sway and surge. The rig with the degrees of freedom can be seen below in Figure 1. Improvement of an existing electronic ride control system (ERCS) allowed the test moth to be able to fly at a range of depth to chord ratios along with the capability to change the respective flight modes with varying amplitudes. Ultimately, it was concluded that in a real-world environment the differences in drag between the range of values tested resulted in no serious measurable performance gains despite significant motion variations. However, it was apparent that small relationships formed and that it is essential for more research to be conducted in order to validate the data. The rig developed provides an easily accessible method for testing control algorithms in a real-world environment without the need for complex sailing configurations. The rig also allows cheap ways of tuning a system that is ripe for full on-water implementation.\",\"PeriodicalId\":367395,\"journal\":{\"name\":\"The 9th Conference on Computational Methods in Marine Engineering (Marine 2021)\",\"volume\":\"103 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2022-01-31\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"The 9th Conference on Computational Methods in Marine Engineering (Marine 2021)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.2218/marine2021.6863\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"The 9th Conference on Computational Methods in Marine Engineering (Marine 2021)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.2218/marine2021.6863","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

摘要

。为了研究改变比例控制系数值对飞行模式的影响,为进一步的数值模拟提供数据,设计、建造和评估了一个测试平台,用于在现实世界条件下测试国际飞蛾级。通过咨询行业、技术专家和查阅文献,我们设计出了一种允许在一系列速度、配置和控制系统下对箔片进行测试的设计,这些系统可以自由地在俯仰和升沉中移动,但在滚转、偏航、摇摆和浪涌中受到限制。在下面的图1中可以看到带有自由度的钻机。对现有电子飞行控制系统(ERCS)的改进使测试飞蛾能够在不同的深度和弦比范围内飞行,并能够根据不同的幅度改变各自的飞行模式。最终得出的结论是,在实际环境中,尽管存在显著的运动变化,但测试值范围之间的阻力差异不会导致严重的可测量性能提升。然而,很明显,形成了小的关系,为了验证数据,有必要进行更多的研究。该平台为在真实环境中测试控制算法提供了一种简便的方法,无需复杂的航行配置。该平台还允许以廉价的方式调整系统,使其成熟,可以完全在水上实施。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Development of a Full Scale Moth Hydrofoil Control System Test Rig
. The design, construction and evaluation of a test platform to test the International Moth class in real world conditions was undertaken with the aim to investigate the effects of altering the value of the proportional control coefficient on flight modes to provide data for further numerical simulations. Through consultation with industry, technical experts and reviews of literature, a design was produced that allowed foils to be tested over a range of velocities, foil configurations and control systems that would be free to move in pitch and heave, however constrained in roll, yaw, sway and surge. The rig with the degrees of freedom can be seen below in Figure 1. Improvement of an existing electronic ride control system (ERCS) allowed the test moth to be able to fly at a range of depth to chord ratios along with the capability to change the respective flight modes with varying amplitudes. Ultimately, it was concluded that in a real-world environment the differences in drag between the range of values tested resulted in no serious measurable performance gains despite significant motion variations. However, it was apparent that small relationships formed and that it is essential for more research to be conducted in order to validate the data. The rig developed provides an easily accessible method for testing control algorithms in a real-world environment without the need for complex sailing configurations. The rig also allows cheap ways of tuning a system that is ripe for full on-water implementation.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信