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| DC 欄位 | 值 | 語言 |
|---|---|---|
| dc.contributor.advisor | 陳志鴻 | zh_TW |
| dc.contributor.advisor | Chih-Hung Chen | en |
| dc.contributor.author | 李宗禧 | zh_TW |
| dc.contributor.author | Tsung-Hsi Lee | en |
| dc.date.accessioned | 2026-02-26T16:50:54Z | - |
| dc.date.available | 2026-02-27 | - |
| dc.date.copyright | 2026-02-26 | - |
| dc.date.issued | 2026 | - |
| dc.date.submitted | 2026-01-29 | - |
| dc.identifier.citation | [1] P. Dickson, Sputnik: The shock of the century. Bloomsbury Publishing USA, 2001.
[2] A. L. Jenks, The cosmonaut who couldn’t stop smiling: the life and legend of Yuri Gagarin. Northern Illinois University Press, 2019. [3] G. Lofgren, H. Schmitt, G. Simmons, and G. Swann, “The apollo 11 samples: Introduction,” in Apollo 11 Lunar Science Conference, Pergamon Press, 1970. [4] M. K. D. Cross and S. M. Pekkanen, “Introduction –space diplomacy: The final frontier of theory and practice,” The Hague Journal of Diplomacy, vol. 18, no. 2–3, pp. 193–217, 2023. [5] M. Smith, D. Craig, N. Herrmann, et al., “The artemis program: An overview of nasa’s activities to return humans to the moon,” in 2020 IEEE aerospace conference, IEEE, 2020, pp. 1–10. [6] Wikimedia Commons. “File: Artemis phase 1.jpg,” Wikipedia. (Aug. 2024), [Online]. Available: https://commons.wikimedia.org/w/index.php?title=File:Artemis_Phase_1.jpg&oldid=910751302 (accessed: 04/21/2025). [7] 行政院科技會報DIGI+. “太空旅行不是夢！一張圖看懂台灣人造衛星30 年發展史,” 未來城市FutureCity ＠天下. (Dec. 2020), [Online]. Available:https://futurecity.cw.com.tw/article/1805 (accessed: 08/24/2025). [8] Wikimedia Commons. “File:intuitive machines＇nova-c lunar lander (im 00309).jpg,”Wikipedia. (Mar. 2025), [Online]. Available: https : / / commons . wikimedia .org/w/index.php?title=File:Intuitive_Machines%E2%80%99_Nova-C _ lunar _ lander _ (IM _ 00309 ) _(cropped ) .jpg & oldid = 1007028175 (accessed:11/06/2025). [9] M. Abedi, T. Jin, and K. Sun, “GNSS signal tracking performance improvement for highly dynamic receivers by gyroscopic mounting crystal oscillator,” Sensors (Basel, Switzerland), vol. 15, no. 9, pp. 21 673–21 695, 2015. [10] S. Zhang, R. F. Wimmer-Schweingruber, J. Yu, et al., “First measurements of the radiation dose on the lunar surface,” Science Advances, vol. 6, no. 39, eaaz1334, 2020. [11] A. Zakharov, L. Zelenyi, and S. Popel＇, “Lunar dust: Properties and potential hazards,” Solar System Research, vol. 54, no. 6, pp. 455–476, 2020. [12] A. R. Vasavada, D. A. Paige, and S. E. Wood, “Near-surface temperatures on mercury and the moon and the stability of polar ice deposits,” Icarus, vol. 141, no. 2, pp. 179–193, 1999. [13] D. Paige, M. Foote, B. Greenhagen, et al., “The lunar reconnaissance orbiter diviner lunar radiometer experiment,” Space Science Reviews, vol. 150, pp. 125–160, 2010. [14] J.-F. Castet and J. H. Saleh, “Satellite reliability: Statistical data analysis and modeling,” Journal of Spacecraft and Rockets, vol. 46, no. 5, pp. 1065–1076, 2009. [15] D. Maisonnier, “Rami: The main challenge of fusion nuclear technologies,” Fusion Engineering and Design, vol. 136, pp. 1202–1208, 2018. [16] P. Fortescue, G. Swinerd, and J. Stark, Spacecraft systems engineering. John Wiley & Sons, 2011. [17] A. K. Sehgal, C. Juneja, J. Singh, and S. Kalsi, “Comparative analysis and review of materials properties used in aerospace industries: An overview,” Materials Today: Proceedings, vol. 48, pp. 1609–1613, 2022. [18] J. Eickhoff, Simulating spacecraft systems. Springer Science & Business Media, 2009. [19] V. Somashekar, S. Harikrishnan, P. A. Ahmed, and D. Kamesh, “Vibration response prediction of the printed circuit boards using experimentally validated finite element model,” Procedia Engineering, vol. 144, pp. 576–583, 2016. [20] D. Ewins, Modal Testing: Theory, Practice and Application. Wiley, 2000. [21] J. K. Sharma, “Theoretical and experimental modal analysis of beam,” in Engineering Vibration, Communication and Information Processing: ICoEVCI 2018, India, Springer, 2018, pp. 177–186. [22] L. Thimmaraju Girijadevi, “Vibration analysis and testing of a 6u cubesat propulsion system,” M.S. thesis, KTH Royal Institute of Technology, 2023. [23] K. Ogawa, Y. Iijima, N. Sakatani, H. Otake, and S. Tanaka, “A thermal control system for long-term survival of scientific instruments on lunar surface,” Review of Scientific Instruments, vol. 85, no. 3, 2014. [24] P. B. Hager, “Dynamic thermal modeling for moving objects on the moon,” Ph.D. dissertation, Technische Universität München, 2013. [25] E. Chuvieco, Fundamentals of satellite remote sensing: An environmental approach. CRC Press, 2020. [26] R. Dunwoody, J. Reilly, D. Murphy, et al., “Thermal vacuum test campaign of the eirsat-1 engineering qualification model,” Aerospace, vol. 9, no. 2, p. 99, 2022. [27] H. Daneshvar, K. G. Milan, A. Sadr, S. H. Sedighy, S. Malekie, and A. Mosayebi, “Multilayer radiation shield for satellite electronic components protection,” Scientific Reports, vol. 11, no. 1, p. 20 657, 2021. [28] O. Bannova and L. Bell, “Radiation shielding design strategies for lunar minimal functionality habitability element,” Acta Astronautica, vol. 67, no. 9-10, pp. 1103–1109, 2010. [29] L. Ding, R. Zhou, T. Yu, et al., “Lunar rock investigation and tri-aspect characterization of lunar farside regolith by a digital twin,” Nature Communications, vol. 15, no. 1, p. 2098, 2024. [30] C. Pieters, S. Besse, J. Boardman, et al., “Mg-spinel lithology: A new rock type on the lunar farside,” Journal of Geophysical Research: Planets, vol. 116, no. E6, 2011. [31] H. Jones, “Moon base life support design depends on launch cost, crew size, and mission duration,” in 49th International Conference on Environmental Systems, 2019. [32] P. T. Metzger and G. W. Autry, “The cost of lunar landing pads with a trade study of construction methods,” New Space, vol. 11, no. 2, pp. 94–123, 2023. [33] Z. Jiao, L. Jiang, J. Sun, J. Huang, and Y. Zhu, “Outgassing environment of spacecraft: An overview,” in IOP Conference Series: Materials Science and Engineering, IOP Publishing, vol. 611, 2019, p. 012 071. [34] J. Garrett, A. Glassford, and J. Steakley, “Astm e 1559 method for measuring material outgassing/deposition kinetics,” Journal of the IES, vol. 38, no. 1, pp. 19–28, 1995. [35] M. F. Diaz-Aguado, J. Greenbaum, W. T. Fowler, and E. G. Lightsey, “Small satellite thermal design, test, and analysis,” in Modeling, Simulation, and Verification of Space-based Systems III, SPIE, vol. 6221, 2006, pp.74–85. [36] J.-R. Tsai, “Overview of satellite thermal analytical model,” Journal of Spacecraft and Rockets, vol. 41, no. 1, pp. 120–125, 2004. [37] M. A. McCullar, “Thermal vacuum testing: Test preparation,” in Proc. Thermal Fluids Anal. Workshop (TFAWS 2010), 2010. [38] E. Petersen, Single event effects in aerospace. John Wiley & Sons, 2011. [39] H. J. Barnaby, “Total-ionizing-dose effects in modern cmos technologies,” IEEE transactions on nuclear science, vol. 53, no. 6, pp. 3103–3121, 2006. [40] A. Sharma, H. Bhojraj, V. Kaila, and H. Narayanamurthy, “Anodizing and inorganic black coloring of aluminum alloys for space applications,” Metal Finishing, vol. 95, no. 12, pp. 14–20, 1997. [41] W. A. Campbell, Outgassing data for selecting spacecraft materials. National Aeronautics and Space Administration, 1987, vol. 1124. [42] J. W. Sheffield and H. J. Sauer, “Thermal contact resistance (tcr)/thermal contact conductance (tcc),” in Heat Exchanger Design Handbook 2008, 2008. [43] E. Grün, M. Horanyi, and Z. Sternovsky, “The lunar dust environment,” Planetary and Space Science, vol. 59, no. 14, pp. 1672–1680, 2011. [44] T. J. Stubbs, R. R. Vondrak, and W. M. Farrell, “Impact of dust on lunar exploration,” in Dust in planetary systems, vol. 643, 2007, pp. 239–243. [45] ECSS, Mechanical Shock Design and Verification Handbook. esa-estec, 2015. [46] C. O. Ayieko, R. J. Musembi, A. A. Ogacho, B. O. Aduda, B. M. Muthoka, and P. K. Jain, “Controlled texturing of aluminum sheet for solar energy applications,” Advances in Materials Physics and Chemistry, vol. 5, no. 11, pp. 458–466, 2015. [47] J. R. Wertz, W. J. Larson, D. Kirkpatrick, and D. Klungle, Space mission analysis and design. Springer, 1999, vol. 8. [48] G. F. Abdelal, N. Abuelfoutouh, and A. H. Gad, Finite Element Analysis for Satellite Structures: Applications to Their Design, Manufacture and Testing. Springer London, 2013. [49] G. Zheng, H. Nie, J. Chen, C. Chen, and H. P. Lee, “Dynamic analysis of lunar lander during soft landing using explicit finite element method,” Acta Astronautica, vol. 148, pp. 69–81, 2018. [50] A. Calvi, “Spacecraft structural dynamics & loads: An overview,” European Space Agency, Tech. Rep., 2010. [51] A. Almesmari, F. Jarrar, F. Almaskari, P. Marpu, N. Abdul Shukoor, and J. Govindan, “Validation and verification of a nanosatellite passive isolator for pyroshock attenuation,” CEAS Space Journal, vol. 13, pp. 133–143, 2021. [52] G. P. Cimellaro and S. Marasco, “Mdof systems,” in Introduction to Dynamics of Structures and Earthquake Engineering. Springer International Publishing, 2018, pp. 95–160. [53] E. Bramanti, G. Cervino, F. Lauritano, et al., “Fem and von mises analysis on prosthetic crowns structural elements: Evaluation of different applied materials,” The Scientific World Journal, vol. 2017, no. 1, p. 1 029 574, 2017. [54] S. Amstutz and A. A. Novotny, “Topological optimization of structures subject to von mises stress constraints,” Structural and Multidisciplinary Optimization, vol. 41, pp. 407–420, 2010. [55] A. Chandra, D. Pathiwada, and S. Chattopadhyay, “Comsol simulation and experimental validation of promoter geometries facilitating citric acid transport in electrodialysis,” Chemical Engineering Research and Design, vol. 142, pp. 386–411, 2019. [56] S. Chaphalkar, S. N. Khetre, and A. M. Meshram, “Modal analysis of cantilever beam structure using finite element analysis and experimental analysis,” American Journal of Engineering Research, vol. 4, no. 10, pp. 178–185, 2015. [57] B. Spieß, K. Höschler, and M. Fanter, A Feature-Based Approach for an Automated Simplification of Structural Aero Engine Components. Deutsche Gesellschaft für Luft-und Raumfahrt-Lilienthal-Oberth eV, 2020. [58] M. G. Pike, D. X. Feng, and M. R. Myers, “Shrinkwrap geometry defeaturing for finite element analysis for a wheel and hub model,” Computer-Aided Design and Applications, vol. 13, no. 3, pp. 295–308, 2016. [59] U. H. Kalyani and M. Wylie, “Modal finite element analysis of pcbs and the role of material anisotropy,” Vibroengineering Procedia, vol. 32, pp. 75–80, 2020. [60] J. Herrera-Arroyave, B. Bermúdez-Reyes, J. Ferrer-Pérez, and A. Colín, “Cubesat system structural design,” in 67th International Astronautical Congress. Guadalajara, Mexico, 2016, pp. 1–5. [61] P. Wen, G. Tao, D. E. Spearot, and S. R. Phillpot, “Molecular dynamics simulation of the shock response of materials: A tutorial,” Journal of Applied Physics, vol. 131, no. 5, 2022. [62] C. Lundergan and W. Herrmann, “Equation of state of 6061-t6 aluminum at low pressures,” Journal of Applied Physics, vol. 34, no. 7, pp. 2046–2052, 1963. [63] J. S. Milne Jr and D. S. Kaufman, “General environmental verification specification,” in 21st Aerospace Testing Seminar, 2003. | - |
| dc.identifier.uri | http://tdr.lib.ntu.edu.tw/jspui/handle/123456789/101703 | - |
| dc.description.abstract | 隨著全球太空探索進入商業化與多國合作的新時代，月球探測再次成為各國發展的重點。本研究為國家太空中心「外太空探索計畫第一枚月球漫遊車（OSE-LR1）酬載儀器研製」計畫之一環，透過產學合作的架構執行，旨在建立臺灣自主開發月球表面科學儀器之能力。此任務的挑戰在於酬載需克服從地表發射到月球表面執行任務過程中的嚴苛環境，包括發射階段的劇烈振動與衝擊，以及月球表面極端的溫差、宇宙輻射與月球塵土（Lunar Dust）等威脅。為應對上述的挑戰，本研究透過有限元素分析（Finite Element Analysis, FEA）軟體，對酬載結構進行負載模擬與設計改良，並藉由一系列環境測試驗證其可靠性（Reliability）。數值分析的重點為模擬酬載於發射與著陸過程中承受的準靜態（Quasi-static）、正弦振動（Sine Vibration）、隨機振動（Random Vibration）與衝擊（Shock）等動態負載，並初步評估月球表面作業的高低溫環境影響。根據分析結果，針對結構弱點進行改良，如提升主結構之自然頻率和優化內部模組配置以增強整體剛性等。最終，依循計畫的規範，透過振動、衝擊、熱真空與輻射等一系列環境測試，驗證酬載設計具備承受任務所需負載的能力。本研究不僅完成了一套符合月球探測任務標準的酬載結構設計，也為臺灣自主開發太空酬載建立了一套完整的設計、分析與驗證流程。 | zh_TW |
| dc.description.abstract | As global space exploration enters a new era of commercialization and international collaboration, lunar missions have once again become a strategic focus. This research, conducted under an industry-academia framework for the Taiwan Space Agency's (TASA) OSE-LR1 lunar rover program, aims to establish Taiwan's capability for the indigenous development of lunar surface scientific instruments.
The primary challenge of this mission lies in ensuring the payload can withstand harsh environments, ranging from severe vibrations and shocks during launch to extreme temperature fluctuations, cosmic radiation, and lunar dust on the lunar surface. To address these challenges, this study employed Finite Element Analysis (FEA) to perform load simulations and structural optimization, followed by a series of environmental tests to verify reliability. The numerical analysis focused on simulating dynamic loads during launch and landing—specifically quasi-static, sine vibration, random vibration, and shock conditions—while providing a preliminary assessment of the lunar thermal environment. Based on the analysis results, structural enhancements were implemented, such as increasing the natural frequency of the main structure and optimizing internal module layout to improve overall stiffness. Finally, the design was validated through a rigorous environmental testing campaign, including vibration, shock, thermal vacuum, and radiation tests, as prescribed by mission standards. This study successfully developed a lunar-qualified payload structure and established a comprehensive design, analysis, and verification workflow for indigenous space payloads in Taiwan. | en |
| dc.description.provenance | Submitted by admin ntu (admin@lib.ntu.edu.tw) on 2026-02-26T16:50:54Z No. of bitstreams: 0 | en |
| dc.description.provenance | Made available in DSpace on 2026-02-26T16:50:54Z (GMT). No. of bitstreams: 0 | en |
| dc.description.tableofcontents | 口試委員審定書 i
誌謝 ii 摘要 iv Abstract v 目次 vii 圖次 x 表次 xiv 第一章 緒論 1 1.1 研究背景 1 1.2 研究動機 4 1.3 文獻探討 9 1.3.1 可靠度與系統工程 9 1.3.2 結構、熱控的設計與驗證 12 1.3.3 環境測試與應對策略 13 1.4 論文架構 16 第二章 光譜影像酬載設計 17 2.1 科學目標與系統架構 17 2.2 酬載系統與環測規格 21 2.3 酬載結構與次系統設計 23 2.3.1 光譜影像酬載主結構設計 27 2.3.2 可見光成像次系統設計 32 2.3.3 多光譜探測次系統設計 36 2.3.4 控制管理次系統設計 48 第三章 數值分析與結果 53 3.1 數值分析方法 54 3.2 數值分析設定 60 3.3 酬載零件分析與改良 62 3.4 酬載結構特性分析 73 3.5 酬載環境測試分析 78 第四章 環境測試驗證 90 4.1 結構領域測試 92 4.2 熱控領域測試 97 4.3 輻射領域測試 101 第五章 結果討論與未來工作 105 5.1 結果討論 105 5.1.1 規格與科學目標達成評估 105 5.1.2 數值分析與實驗比較 106 5.1.3 結論 107 5.2 未來工作 109 參考文獻 111 附錄A — 初步熱傳分析結果117 A.1 熱傳分析邊界條件 117 A.2 分析結果與討論 118 | - |
| dc.language.iso | zh_TW | - |
| dc.subject | 月球漫遊車酬載 | - |
| dc.subject | 有限元素法 | - |
| dc.subject | COMSOL多物理場模擬軟體 | - |
| dc.subject | 結構設計 | - |
| dc.subject | 數值分析 | - |
| dc.subject | 應力應變分析 | - |
| dc.subject | 環境測試 | - |
| dc.subject | Payload of Lunar Rover | - |
| dc.subject | Finite Element Method | - |
| dc.subject | COMSOL Multiphysics | - |
| dc.subject | Structural Design | - |
| dc.subject | Numerical Analysis | - |
| dc.subject | Stress-strain Analysis | - |
| dc.subject | Environmental Test | - |
| dc.title | 月球漫遊車光譜影像酬載結構設計與數值分析 | zh_TW |
| dc.title | Structural Design and Numerical Analysis of the Multispectral and Imaging Payload on a Lunar Rover | en |
| dc.type | Thesis | - |
| dc.date.schoolyear | 114-1 | - |
| dc.description.degree | 碩士 | - |
| dc.contributor.oralexamcommittee | 周佳靚;柯正浩;許軒豪 | zh_TW |
| dc.contributor.oralexamcommittee | Chia-Ching Chou;Cheng-Hao Ko;Shiuan-Hal Shiu | en |
| dc.subject.keyword | 月球漫遊車酬載,有限元素法COMSOL多物理場模擬軟體結構設計數值分析應力應變分析環境測試 | zh_TW |
| dc.subject.keyword | Payload of Lunar Rover,Finite Element MethodCOMSOL MultiphysicsStructural DesignNumerical AnalysisStress-strain AnalysisEnvironmental Test | en |
| dc.relation.page | 121 | - |
| dc.identifier.doi | 10.6342/NTU202504649 | - |
| dc.rights.note | 同意授權(全球公開) | - |
| dc.date.accepted | 2026-01-30 | - |
| dc.contributor.author-college | 工學院 | - |
| dc.contributor.author-dept | 應用力學研究所 | - |
| dc.date.embargo-lift | 2030-12-15 | - |
| 顯示於系所單位： | 應用力學研究所 | |
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