博碩士論文 111353031 詳細資訊




以作者查詢圖書館館藏 以作者查詢臺灣博碩士 以作者查詢全國書目 勘誤回報 、線上人數:52 、訪客IP:18.191.233.51
姓名 周慈萱(Tzu-Hsien Chou)  查詢紙本館藏   畢業系所 機械工程學系在職專班
論文名稱 深太空輻射探測儀的靜態和動態分析
(Static and Dynamic Analysis of The Deep Space Radiation Probe)
檔案 [Endnote RIS 格式]    [Bibtex 格式]    [相關文章]   [文章引用]   [完整記錄]   [館藏目錄]   至系統瀏覽論文 (2027-7-24以後開放)
摘要(中) 由國立中央大學師生開發的深太空輻射探測儀(Deep Space Radiation Probe, 簡稱DSRP)準備加入日本民間ispace的Hakuto-R Mission 2(M2)登月任務,將過去累積的IDEASSat任務開發經驗結合加以改良的游離輻射容忍度,深入了解太空輻射環境對立方衛星的影響。本論文聚焦於使用有限元素分析(FEA)軟體ANSYS Workbench和電腦輔助設計(CAD)軟體SolidWorks對該酬載工程體進行數值模擬分析,包含線性靜態的等效應力、等效應變和總變形分析,以及線性動態的自然頻率、模態與隨機振動分析。為了對比兩種不同類型軟體的模擬功能,本研究將動態模擬結果與先前研究中之振動實驗的結果進行比對和驗證,模擬結果與實驗結果大致吻合。但發現SolidWorks較適合初學者創建零組件,其內建的有限元素求解器在材料和網格的選擇上較少,導致分析時間較短,結果也較不精確;而ANSYS Workbench則具備混合式網格劃分和精確的準靜態模擬選項,其數值模擬結果與先前研究中的實驗結果一致性頗高,顯示其準確性。此分析技術與經驗可以提供小型酬載更準確的數值數據和更方便的模擬程序,此外,本研究也針對未來深太空輻射探測儀飛行體提出對應的結構改善方案。
摘要(英) The Deep Space Radiation Probe (DSRP) developed by the students and faculty of National Central University is scheduled to land on the Moon with ispace Hakuto-R Mission 2 (M2). It is hoped to characterize the deep space radiation environment to quantify its effect on spacecraft electronics and biological organisms. This thesis project concentrates on comparing numerical analysis solutions of the DSRP engineering model, using finite element analysis (FEA) software ANSYS Workbench and computer-aided design (CAD) software SolidWorks. The studied events are focused on the linear quasi-static analysis of equivalent stress, equivalent strain, and total deformation, as well as, linear dynamic analysis of natural frequencies, mode shapes, and random vibration. The idea is to understand better the functions and results produced by the two types of software and to utilize the results to determine the possible improvement for future DSRP structural design. The numerical results of natural frequencies and mode shapes, and random vibration analysis are verified using experimental vibration testing results from the previous studies. A comparison between the two analysis tools shows that SolidWorks is intended to allow relatively inexperienced users to quickly and easily create 3D parts. Its built-in FEA solver has a relatively simpler material library and meshing techniques. However, ANSYS Workbench has hybrid meshing and quasi-static options which can provide more accurate and consistent FEA solutions. Using models built from SolidWorks in linear static and dynamic analysis in ANSYS Workbench for future small payloads will save the design team the stress of manufacturing multiple models before the system gets qualified.
關鍵字(中) ★ 深太空輻射探測儀
★ 有限元素分析
★ ANSYS Workbench
★ SolidWorks
★ 線性靜態
★ 線性動態
關鍵字(英) ★ Deep Space Radiation Probe
★ finite element analysis
★ ANSYS Workbench
★ SolidWorks
★ quasi-static analysis
★ linear dynamic analysis
論文目次 摘要 ................................................. i
Abstract ......................................... ii
誌謝 ............................................... iii
Table Of Contents ....................... iv
List Of Figures ............................. vi
List Of Tables............................................... xviii
Chapter 1. Introduction ................ 1
1-1 Loads on The Spacecraft Structure ........... 2
1-2 Vibration Testing of Spacecraft Structures ....................................... 4
1-3 Quasi-Static Testing of Spacecraft Structures .................................. 6
1-4 Introduction to Deep Space Radiation Probe ................................... 7
1-5 The DSRP Engineering and Flight Models ...................................... 9
Chapter 2. Theory of Mechanical Vibrations ....................................... 12
2-1 Introduction ......................... 12
2-2 Dynamic Analysis ............... 13
2-2-1 Equations and Solution Procedures of Dynamic Analysis ... 15
2-2-2 Natural Frequencies and Mode Shapes ................................. 16
2-2-3 Modal Analysis................... 18
2-2-4 Damping ....................... 19
2-3 Random Vibration.......................... 20
2-4 Quasi-Static Analysis.......................... 23
Chapter 3. Procedures of Static and Dynamic Analysis Using Numerical Simulation .................... 24
3-1 Finite Element Method And Simulation Procedures ...................... 25
3-1-1 Finite Element Models Establishment .................................. 26
3-1-2 Material Selection .............. 30
3-1-3 Loadings of Structural Analysis ............................................ 33
3-1-4 Boundary Conditions ...... 34
3-1-5 Mesh Convergence Study ..................................................... 42
3-2 Quasi-Static Analysis........................ 42
3-2-1 Static Structural Analysis in Ansys ....................................... 42
3-2-2 Static Analysis in Solidworks ............................................... 53
3-3 Dynamic Analysis-Natural Frequencies And Mode Shapes. 66
3-3-1 Modal Analysis in Ansys .... 66
3-3-2 Frequency Analysis in Solidworks ................. 78
3-4 Dynamic Analysis-Random Vibrations ................ 89
3-4-1 Random Vibration Analysis in Ansys ................................... 90
3-4-2 Random Vibration Analysis in Solidworks........... 92
Chapter 4. Vibration Tests of The Deep Space Radiation Probe ....... 95
4-1 Environmental Test Specifications .................. 96
4-2 Response of Natural Frequency Survey................ 98
4-3 Results of Random Vibration Tests.................. 100
Chapter 5. Results and Discussions..................... 101
5-1 Comparison of Finite Element Models .............. 101
5-2 Comparison of Quasi-Static Analysis in X, Y, And Z Axes ......... 110
5-3 Comparison of Numerical Simulation of Dynamic Analysis and Vibration Test Results....................... 112
5-3-1 Mode Shapes And Natural Frequencies in Z-Axis Direction . 112
5-3-2 Random Vibration in Z-Axis Direction ......... 127
Chapter 6. Conclusions and Future Developments........ 132
6-1 Conclusions....................................... 132
6-2 Future Developments .............................. 134
Bibliography ...................................................... 136
參考文獻 [1] ispace.inc., 2024, [accessed June 20, 2024]; Available from: https://ispace-inc.com/aboutus.
[2] Yunis, I., 2005, "The Standard Deviation of Launch Vehicle Environments, in AIAA Structures, Structural Dynamics, and Materials Conference." , American Inst. of Aeronautics and Astronautics: NASA Kennedy Space Centre Cocoa Beach, FL, United States.
[3] SachithWarnakulasuriya, H., 2021, "Vibration Analysis and Testing of a Satellite Structure during it’s Launch and In-flight Stages.," University of Twente. p. 88.
[4] Date, T., et al., 2022, "NCU Payload Interface Requirement Document M2-RSP-PL-00003 Issue 01 Revision 01."
[5] Cruise, A.M., et al, Bowles, J.A., Patrick, T.J., and Goodall, C.V, 1998, "Principles of Space Instrument Design", Cambridge: Cambridge University Press.
[6] Yilmaz, F., O.O. Haktanir, and A.B. Uygur, 2015, "Quasi-Static Structural Test of Satellites. in 2015 7th International Conference on Recent Advances in Space Technologies (RAST)."
[7] Chang, L.C., et al., 2024, "The Deep Space Radiation Probe: Development of a First Lunar Science Payload for Space Environment Studies and Capacity Building." Advances in Space Research.
137
[8] ispace.inc., 2023, [accessed June 18, 2024]; Available from: https://ispace-inc.com/news-en/?p=4401.
[9] Ltd, V., 2023, "Technical Data RM-VT01-A VT01 RADFET Readout Module Revision 1.3."
[10] Heidecker, J., 2012, "NAND flash screening and qualification guideline for space application.," Available from: https://dataverse.jpl.nasa.gov/dataset.xhtml?persistentId=hdl:2014/41965.
[11] Microchip Technology, inc., 2023, "SmartFusion® 2 FPGAs., "[acceessed 1 July, 2024]; Available from: https://www.microchip.com/en-us/products/fpgas-and-plds/system-on-chip-fpgas/smartfusion-2-fpgas.
[12] Chang, L.C., et al., 2023, "DSRP-EIDP Issue 00 Revision 00."
[13] AUTODESK., [None], "AUTODESK Structural Bridge Design 2025." [accessed 26 May, 2024]; Available from: https://help.autodesk.com/view/SBRDES/ENU/?guid=ASBD_InProdEU_structure_tech_info_ti_dynamics_Dynamic_Analysis_Introduction_html.
[14] Rao, S.S., 2018, "Mechanical Vibrations." Sixth edition in SI units ed. , Harlow, England: Pearson.
[15] Ontaç, S., 2008, "Finite Element Analysis of a Micro Satellite Structure Under Vibration Induced Loads During Launch, in Graduate School of Natural and Applied Sciences.," Middle East Technical University.
138
[16] Bolognese, J. and Simmons, R., 2009, "Calulating Grms (Root-Mean-Square Acceleration)", [accessed 6 May, 2024]; Available from: https://femci.gsfc.nasa.gov/random/randomgrms.html.
[17] Girijadevi, L.T., 2023, "Vibration analysis and testing of a 6U cubesat propulsion system," in School of Engineering Sciences., KTH Royal Institute of Technology: Uppsala, Sweden.
[18] ANSYS, inc., ANSYS 2021 R2., 2021, ANSYS, Inc.: Canonsburg, PA.
[19] Dassault Systèmes, 2019, "SolidWorks 2020," Dassault Systèmes: Waltham, MA.
[20] Wang, D., Liu, X., Chen, S. and Jiang, D., 2023, "Static and Vibration Analysis of Manned Lunar Rover Frame Based on Ansys," 6th International Conference on Electronics Technology (ICET). p. 886-891.
[21] Hemesh, P. and P.V. Jeyakarthikeyan, 2018, "Mesh Convergence Study and Estimation of Discretization Error of Hub in Clutch Disc with Integration of ANSYS." IOP Conference Series: Materials Science and Engineering, 402(1): p. 012065.
[22] Ralph R., Roe, J., 2022, "Structural Design and Test Factors of Safety for Spaceflight Hardware."
[23] Chang, L.C., et al., 2023, "DSRP-STR-PROC Issue 00 Revision 00."
[24] [None], 2024, "Mesh Quality Checks.," [accessed June 10,2024]; Available from:
139
https://help.solidworks.com/2024/english/SolidWorks/cworks/c_mesh_quality_checks.htm.
[25] Hou, K.-J., 2023, "Design, Simulation, Test and Verification of Deep Space Radiation Probe Structure and Thermal Control.," National Central University: Taiwan. p. 228.
[26] Mantovani, J., [None],"Preprocessing.," Topics relate to geometry, meshing and CAD 2020, [accessed 2024 June 20]; Available from: https://forum.ansys.com/forums/topic/what-is-the-source-of-mesh-quality-spectrum/.
指導教授 黃以玫 張起維(YiMei Huang Loren C. Chang) 審核日期 2024-8-17
推文 facebook   plurk   twitter   funp   google   live   udn   HD   myshare   reddit   netvibes   friend   youpush   delicious   baidu   
網路書籤 Google bookmarks   del.icio.us   hemidemi   myshare   

若有論文相關問題,請聯絡國立中央大學圖書館推廣服務組 TEL:(03)422-7151轉57407,或E-mail聯絡  - 隱私權政策聲明