{"title":"Design optimization of a hexapod vibration isolation system for electro-optical payload","authors":"Jing LI, Weipeng LI, Xiaoyan ZHANG, Hai HUANG","doi":"10.1016/j.cja.2023.12.003","DOIUrl":null,"url":null,"abstract":"<div><p>The electro-optical payloads on mobile platforms generally suffer undesirable vibrations generated by maneuvers and turbulence. These vibrations are in six degrees of freedom and cause line-of-sight jitters, resulting in image blurring and loss of tracking accuracy. In this paper, a Hexapod Vibration Isolation System (HVIS) is proposed and optimized to solve this problem. The optimization aims to centralize and minimize the natural frequencies of HVIS, for expanding the vibration isolation bandwidth and improving the vibration isolation in the higher frequency band. Considering that the design space for HVIS is limited and interfered with the frames of the mobile platform, a non-collision algorithm is proposed and applied in the optimization to obtain the feasible optimal design. The optimization result shows that the natural frequency bandwidth has been reduced by 42.9 %, and the maximum natural frequency is reduced by 30.2 %. The prototypes of initial and optimal designs are manufactured and tested. Both simulated and experimental results demonstrate the validity of the optimization, and the optimal design provides a maximum of 15 dB more isolation in rotation direction than the initial design.</p></div>","PeriodicalId":55631,"journal":{"name":"Chinese Journal of Aeronautics","volume":"37 2","pages":"Pages 330-342"},"PeriodicalIF":5.3000,"publicationDate":"2023-12-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S1000936123004181/pdfft?md5=2dc8d7d4fb033c58e4d9eb1794748338&pid=1-s2.0-S1000936123004181-main.pdf","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Chinese Journal of Aeronautics","FirstCategoryId":"1087","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1000936123004181","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0
Abstract
The electro-optical payloads on mobile platforms generally suffer undesirable vibrations generated by maneuvers and turbulence. These vibrations are in six degrees of freedom and cause line-of-sight jitters, resulting in image blurring and loss of tracking accuracy. In this paper, a Hexapod Vibration Isolation System (HVIS) is proposed and optimized to solve this problem. The optimization aims to centralize and minimize the natural frequencies of HVIS, for expanding the vibration isolation bandwidth and improving the vibration isolation in the higher frequency band. Considering that the design space for HVIS is limited and interfered with the frames of the mobile platform, a non-collision algorithm is proposed and applied in the optimization to obtain the feasible optimal design. The optimization result shows that the natural frequency bandwidth has been reduced by 42.9 %, and the maximum natural frequency is reduced by 30.2 %. The prototypes of initial and optimal designs are manufactured and tested. Both simulated and experimental results demonstrate the validity of the optimization, and the optimal design provides a maximum of 15 dB more isolation in rotation direction than the initial design.
移动平台上的电子光学有效载荷通常会受到机动和湍流产生的不良振动的影响。这些振动具有六个自由度,会造成视线抖动,导致图像模糊和跟踪精度下降。本文提出并优化了六足架振动隔离系统(HVIS),以解决这一问题。优化的目的是集中并最小化 HVIS 的固有频率,以扩大隔振带宽并提高高频段的隔振效果。考虑到 HVIS 的设计空间有限且与移动平台的框架相互干扰,提出了一种非碰撞算法并将其应用于优化,以获得可行的最优设计。优化结果表明,固有频率带宽降低了 42.9%,最大固有频率降低了 30.2%。对初始设计和优化设计的原型进行了制造和测试。模拟和实验结果都证明了优化的有效性,与初始设计相比,优化设计在旋转方向上的隔离度最多提高了 15 dB。
期刊介绍:
Chinese Journal of Aeronautics (CJA) is an open access, peer-reviewed international journal covering all aspects of aerospace engineering. The Journal reports the scientific and technological achievements and frontiers in aeronautic engineering and astronautic engineering, in both theory and practice, such as theoretical research articles, experiment ones, research notes, comprehensive reviews, technological briefs and other reports on the latest developments and everything related to the fields of aeronautics and astronautics, as well as those ground equipment concerned.