CLPS月球车GrainCams载荷的初步机械设计

Woojin Kim, B. Moon, Dukhang Lee, Dae-Hee Lee, Min-Bae Kim, M. Jeong, Jihun Kim, Seonghwan Choi, Jehyuck Shin, Mingyeong Lee, S. Baek, C. Sim, Young-Jun Choi, Sungsoo S. Kim
{"title":"CLPS月球车GrainCams载荷的初步机械设计","authors":"Woojin Kim, B. Moon, Dukhang Lee, Dae-Hee Lee, Min-Bae Kim, M. Jeong, Jihun Kim, Seonghwan Choi, Jehyuck Shin, Mingyeong Lee, S. Baek, C. Sim, Young-Jun Choi, Sungsoo S. Kim","doi":"10.1117/12.2677855","DOIUrl":null,"url":null,"abstract":"GrainCams is a lunar rover payload designed to explore lunar dust. It is a suite of two light field cameras: SurfCam and LevCam. The main goal of SurfCam is to provide 3D imaging of fairy castle structures believed to exist on the lunar surface. LevCam’s objective is to understand dust speed and track the trail of lofting dust on the lunar surface. The mechanical stiffness of the camera is capable of enduring the vibration and shock conditions of the launcher. Thus, we conducted the opto-mechanical design for Surfam and analyzed the safety through theoretical estimation. The safety of whole structure is also reviewed from structural analysis such as linear static analysis and modal analysis. These cameras will operate in the extreme temperature of the moon. To achieve a viable thermal design despite the extreme lunar thermal environment and uncertainty of the payload interface with the rover, we assumed a thermal adiabatic payload interface and employed passive (e.g., thermal insulation blankets (MLIs), surface control of thermal radiation, specially designed radiators with an inclination angle of 36.5° to effectively avoid Solar flux and maximize unobstructed view of space relative to the lunar surface in hot cases) and active (e.g., heaters) thermal control techniques. Each camera should weigh no more than 5 kg and consume no more than 20 W of power. In this paper, we present the preliminary results of the structure design of GrainCams.","PeriodicalId":434863,"journal":{"name":"Optical Engineering + Applications","volume":"42 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2023-10-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Preliminary mechanical design of GrainCams payload for the CLPS lunar rover\",\"authors\":\"Woojin Kim, B. Moon, Dukhang Lee, Dae-Hee Lee, Min-Bae Kim, M. Jeong, Jihun Kim, Seonghwan Choi, Jehyuck Shin, Mingyeong Lee, S. Baek, C. Sim, Young-Jun Choi, Sungsoo S. Kim\",\"doi\":\"10.1117/12.2677855\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"GrainCams is a lunar rover payload designed to explore lunar dust. It is a suite of two light field cameras: SurfCam and LevCam. The main goal of SurfCam is to provide 3D imaging of fairy castle structures believed to exist on the lunar surface. LevCam’s objective is to understand dust speed and track the trail of lofting dust on the lunar surface. The mechanical stiffness of the camera is capable of enduring the vibration and shock conditions of the launcher. Thus, we conducted the opto-mechanical design for Surfam and analyzed the safety through theoretical estimation. The safety of whole structure is also reviewed from structural analysis such as linear static analysis and modal analysis. These cameras will operate in the extreme temperature of the moon. To achieve a viable thermal design despite the extreme lunar thermal environment and uncertainty of the payload interface with the rover, we assumed a thermal adiabatic payload interface and employed passive (e.g., thermal insulation blankets (MLIs), surface control of thermal radiation, specially designed radiators with an inclination angle of 36.5° to effectively avoid Solar flux and maximize unobstructed view of space relative to the lunar surface in hot cases) and active (e.g., heaters) thermal control techniques. Each camera should weigh no more than 5 kg and consume no more than 20 W of power. In this paper, we present the preliminary results of the structure design of GrainCams.\",\"PeriodicalId\":434863,\"journal\":{\"name\":\"Optical Engineering + Applications\",\"volume\":\"42 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2023-10-04\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Optical Engineering + Applications\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1117/12.2677855\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Optical Engineering + Applications","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1117/12.2677855","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

“谷物相机”是一种月球探测器,用于探测月球尘埃。它由两个光场相机组成:SurfCam和LevCam。SurfCam的主要目标是提供据信存在于月球表面的童话城堡结构的3D图像。LevCam的目标是了解尘埃的速度,并追踪尘埃在月球表面飞扬的轨迹。相机的机械刚度能够承受发射装置的振动和冲击条件。因此,我们对Surfam进行了光机械设计,并通过理论估计对其安全性进行了分析。从结构分析如线性静力分析和模态分析等方面对结构整体的安全性进行了综述。这些相机将在月球的极端温度下工作。为了在极端的月球热环境和与月球车的有效载荷界面不确定的情况下实现可行的热设计,我们假设了一个绝热的有效载荷界面,并采用了被动(如隔热毯(MLIs))、表面热辐射控制、专门设计的倾角为36.5°的散热器,以有效避免太阳通量,并在炎热的情况下最大限度地获得相对于月球表面的无遮挡空间视图)和主动(如:加热器)热控制技术。每台摄像机重量不超过5kg,功耗不超过20w。在本文中,我们给出了颗粒凸轮结构设计的初步结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Preliminary mechanical design of GrainCams payload for the CLPS lunar rover
GrainCams is a lunar rover payload designed to explore lunar dust. It is a suite of two light field cameras: SurfCam and LevCam. The main goal of SurfCam is to provide 3D imaging of fairy castle structures believed to exist on the lunar surface. LevCam’s objective is to understand dust speed and track the trail of lofting dust on the lunar surface. The mechanical stiffness of the camera is capable of enduring the vibration and shock conditions of the launcher. Thus, we conducted the opto-mechanical design for Surfam and analyzed the safety through theoretical estimation. The safety of whole structure is also reviewed from structural analysis such as linear static analysis and modal analysis. These cameras will operate in the extreme temperature of the moon. To achieve a viable thermal design despite the extreme lunar thermal environment and uncertainty of the payload interface with the rover, we assumed a thermal adiabatic payload interface and employed passive (e.g., thermal insulation blankets (MLIs), surface control of thermal radiation, specially designed radiators with an inclination angle of 36.5° to effectively avoid Solar flux and maximize unobstructed view of space relative to the lunar surface in hot cases) and active (e.g., heaters) thermal control techniques. Each camera should weigh no more than 5 kg and consume no more than 20 W of power. In this paper, we present the preliminary results of the structure design of GrainCams.
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:604180095
Book学术官方微信