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| DC 欄位 | 值 | 語言 |
|---|---|---|
| dc.contributor.advisor | 楊士進 | zh_TW |
| dc.contributor.advisor | Shih-Chin Yang | en |
| dc.contributor.author | 呂柏廷 | zh_TW |
| dc.contributor.author | Bo-Ting Lyu | en |
| dc.date.accessioned | 2024-08-16T16:53:02Z | - |
| dc.date.available | 2024-08-17 | - |
| dc.date.copyright | 2024-08-16 | - |
| dc.date.issued | 2024 | - |
| dc.date.submitted | 2024-08-06 | - |
| dc.identifier.citation | [1] Y. He, S. Yang, S. Lin, W. He, and Z. Yang, "Satellite Attitude Control for Emergency Mode Using Reaction Wheels and Magnetic Torquers," in 2023 6th International Conference on Robotics, Control and Automation Engineering (RCAE), 3-5 Nov. 2023 2023, pp. 207-211, doi: 10.1109/RCAE59706.2023.10398835.
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Chung, "Novel Four-Phase Spherical Reaction Wheel Motor with Vector Control for Three-DOF CubeSat Attitude Determination and Control System," in IECON 2023- 49th Annual Conference of the IEEE Industrial Electronics Society, 16-19 Oct. 2023 2023, pp. 1-6, doi: 10.1109/IECON51785.2023.10312721. [6] R. Takehana and K. Uchiyama, "Attitude controller design for a small satellite using spherical reaction wheel system," in 2017 11th Asian Control Conference (ASCC), 17-20 Dec. 2017 2017, pp. 1841-1846, doi: 10.1109/ASCC.2017.8287454. [7] S.-H. Lee, H.-H. Seo, and S.-W. Rhee, "Performance Analysis of Magnetic Torquer for Spacecraft Control," presented at the ICCAS2005, Gyeonggi-Do, Korea, 2005. [8] N. Bedrossian, S. Bhatt, W. Kang, and I. Ross, "Zero-propellant maneuver guidance," Control Systems, IEEE, vol. 29, pp. 53-73, 11/01 2009, doi: 10.1109/MCS.2009.934089. [9] D. C. Hsiao and M. F. 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Kubátová, and M. Novotný, "Influence of passive hardware redundancy on differential power analysis resistance of AES cipher implemented in FPGA," Microprocessors and Microsystems, vol. 51, pp. 220-226, 2017/06/01/ 2017, doi: https://doi.org/10.1016/j.micpro.2017.04.014. [26] S. Milano, "Allegro Hall-Effect Sensor ICs." [27] Y. Deguchi, K. Yamamoto, K. Otomo, Y. Nagatsu, and H. Hashimoto, "Evaluation of Magnetic Absolute Encoder Using an Eccentric Structure with Feedback Correction," in IECON 2018 - 44th Annual Conference of the IEEE Industrial Electronics Society, 21-23 Oct. 2018 2018, pp. 3764-3769, doi: 10.1109/IECON.2018.8591365. [28] K. Jankowska and M. Dybkowski, "Classification of Optoelectronic Rotary Encoder Faults Based on Deep Learning Methods in Permanent Magnet Synchronous Motor Drive System," Electronics, vol. 12, no. 19, doi: 10.3390/electronics12194184. [29] J. X. Shen, Z. Q. Zhu, and D. Howe, "PM brushless drives with low-cost and low-resolution position sensors," in The 4th International Power Electronics and Motion Control Conference, 2004. IPEMC 2004., 14-16 Aug. 2004 2004, vol. 2, pp. 1033-1038 Vol.2. [30] X. Zhang and W. Zhang, "An improved rotor position estimation in PMSM with low-resolution hall-effect sensors," in 2014 17th International Conference on Electrical Machines and Systems (ICEMS), 22-25 Oct. 2014 2014, pp. 2722-2727, doi: 10.1109/ICEMS.2014.7013961. [31] N. Muley, A. Saxena, and P. Chaudhary, "Comparative Evaluation of Methods for Continuous Rotor Position Estimation using Low Resolution Hall Sensors," in 2021 National Power Electronics Conference (NPEC), 15-17 Dec. 2021 2021, pp. 1-6, doi: 10.1109/NPEC52100.2021.9672505. [32] Z. Yong, H. Wenxin, Y. Jufeng, B. Feifei, and L. Saide, "A PMSM rotor position estimation with low-cost Hall-effect sensors using improved PLL," in 2016 IEEE Transportation Electrification Conference and Expo, Asia-Pacific (ITEC Asia-Pacific), 1-4 June 2016 2016, pp. 804-807, doi: 10.1109/ITEC-AP.2016.7513058. [33] M. Zhao, Q. An, C. Chen, F. Cao, and S. Li, "Observer Based Improved Position Estimation in Field-Oriented Controlled PMSM with Misplaced Hall-Effect Sensors," Energies, vol. 15, no. 16, doi: 10.3390/en15165985. [34] Q. An, C. Chen, M. Zhao, T. Ma, and K. Ge, "Research on Rotor Position Estimation of PMSM Based on Hall Position Sensor," in 2021 IEEE 16th Conference on Industrial Electronics and Applications (ICIEA), 1-4 Aug. 2021 2021, pp. 2088-2094, doi: 10.1109/ICIEA51954.2021.9516180. [35] G. D. Donato, G. Scelba, M. Pulvirenti, G. Scarcella, and F. G. Capponi, "Low-Cost, High-Resolution, Fault-Robust Position and Speed Estimation for PMSM Drives Operating in Safety-Critical Systems," IEEE Transactions on Power Electronics, vol. 34, no. 1, pp. 550-564, 2019, doi: 10.1109/TPEL.2018.2820042. [36] S. Y. Kim, C. Choi, K. Lee, and W. Lee, "An Improved Rotor Position Estimation With Vector-Tracking Observer in PMSM Drives With Low-Resolution Hall-Effect Sensors," IEEE Transactions on Industrial Electronics, vol. 58, no. 9, pp. 4078-4086, 2011, doi: 10.1109/TIE.2010.2098367. [37] Y. Huang, M. Zhao, J. Zhang, and M. Lu, "The Hall Sensors Fault-Tolerant for PMSM Based on Switching Sensorless Control With PI Parameters Optimization," IEEE Access, vol. 10, pp. 114048-114059, 2022, doi: 10.1109/ACCESS.2022.3218325. [38] M. Ebadpour, N. Amiri, and J. 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Alballa, and A. F. Hashem, "Reliability analysis of the triple modular redundancy system under step-partially accelerated life tests using Lomax distribution," Scientific Reports, vol. 13, no. 1, p. 14719, 2023/09/07 2023, doi: 10.1038/s41598-023-41363-3 | - |
| dc.identifier.uri | http://tdr.lib.ntu.edu.tw/jspui/handle/123456789/94585 | - |
| dc.description.abstract | 本論文提出了一個專為大型衛星應用的軸向磁通馬達(Axial Flux Motor-AFM)反應輪，為了確保衛星系統的高可靠性，本文提出集成的印刷電路板(Printed Circuit Board-PCB)定子繞組取代傳統的漆包線繞組，此 PCB 設計能利用自動化製版工藝使定子繞組安裝精確一致，與傳統銅漆包線繞組相比將製造引發的變異和故障風險降到最低。而 PCB 定子繞組電感與磁通量較低的缺點，可以透過軸向磁通的架構來補償，提升轉矩以及功率密度。
在反應輪驅動方面，霍爾感測器經常被選用來進行馬達角度位置回授，傳統 漆包線繞組需要額外感測器固定治具，降低感測器位置偏差問題。但是透過本論文提出的集成 PCB 電路板硬體，霍爾感測器可以直接利用表面貼焊技術安裝，簡化感測器安裝流程。此外 PCB 硬體的特性可輕易實現兩個獨立霍爾傳感器組的冗餘設計，針對此 PCB 集成優點，本論文提出新型的控制容錯控制方法（Fault Tolerant Control-FTC），能在最多三個霍爾感測器故障情況下確保反應輪穩定運行，使反應輪系統滿足太空環境中具有高可靠性的要求。 本論文製造了一個反應輪雛型體進行測試，經實驗結果證明提出的集成PCB 定子之軸向磁通反應輪在緊湊的體積重量限制下表現出色。提出的雙重冗餘霍爾傳感器設計與容錯控制方法，可使反應輪在霍爾感測器失效時，無論是在旋轉還是靜止啟動狀態下皆能正常工作。 | zh_TW |
| dc.description.abstract | This thesis proposes an axial flux motor (AFM) reaction wheel specifically designed for large satellite applications. An integrated PCB stator winding is proposed to replace the conventional enameled copper winding. The proposed PCB design not only leverages the PCB automation process to achieve the precise wire fabrication but also minimizes potential winding faults caused by conventional cooper winding manufacturing process. The drawback of PCB winding with low inductance and low magnetic flux linkage can be improved by the advanced axial flux motor topology.
Regarding to the reaction wheel motor drive, the installation of Hall effect sensors requires the additional fixture on conventional copper winding to maintain the position measurement accuracy. However, the Hall sensors can be directly mounted on the proposed PCB stator hardware. This fabrication advantage further improves the position sensor reliability on the reaction wheel operation. More importantly, the PCB topology allows the dual-redundant design on Hall sensors. Under this advantage, this thesis proposes a novel fault tolerant control (FTC) . This FTC ensures the stable operation of reaction wheel even with up to three Hall sensor failures. It thereby enhances the overall system stability to meet the demanded satellite reliability requirement. A reaction wheel prototype is also fabricated for the experimental verification. The experimental results demonstrate that the AFM reaction wheel design with the proposed PCB stator performs excellently in a compact volume at lightweight. Moreover, the proposed FTC with dual-redundant Hall sensors can operate normally for the reaction wheel in both rotational and stationary startup states under different Hall sensor failures. | en |
| dc.description.provenance | Submitted by admin ntu (admin@lib.ntu.edu.tw) on 2024-08-16T16:53:02Z No. of bitstreams: 0 | en |
| dc.description.provenance | Made available in DSpace on 2024-08-16T16:53:02Z (GMT). No. of bitstreams: 0 | en |
| dc.description.tableofcontents | 口試委員審定書 i
中文摘要 ii ABSTRACT iii 目次 v 表次 ix 圖次 xi 符號列表 xv 第1章 緒論 1 1.1 研究背景 1 1.2 文獻回顧 3 1.2.1 反應輪馬達在衛星的應用 3 1.2.2 反應輪馬達設計 6 1.2.3 位置感測器介紹 9 1.2.4 霍爾感測器解析度改善 13 1.2.5 霍爾感測器容錯控制 17 1.3 研究目的 23 1.3.1 集成PCB繞線定子設計 23 1.3.2 感測器冗餘設計 23 1.3.3 感測器容錯控制 24 1.4 論文大綱 24 第2章 反應輪馬達設計 25 2.1 反應輪規格分析 25 2.2 反應輪機構設計 27 2.3 反應輪磁路設計 28 2.3.1 繞線方法 29 2.3.2 有限元素法分析 29 2.3.3 線性模型模擬 33 2.4 反應輪定子設計 35 2.5 反應輪樣機測試 38 2.5.1 反電動勢與力矩實驗 39 2.5.2 電流控制實驗 40 2.5.3 速度控制實驗 42 2.5.4 樣機測試小結 42 第3章 霍爾感測器冗餘設計 44 3.1 霍爾感測器失效原因 44 3.2 冗餘設計與可靠度分析 46 3.2.1 分析原理 46 3.2.2 冗餘設計效益比較 48 3.3 霍爾感測器雙重冗餘設計 49 3.3.1 狀態表示方法 49 3.3.2 感測器排列幾何比較 50 3.4 感測器失效模式統計 54 3.4.1 單感測器失效模式統計 54 3.4.2 雙感測器失效模式統計 56 3.4.3 不同排列失效模式比較 59 3.4.4 三感測器失效模式統計 59 3.5 雙重冗餘設計應用 62 第4章 霍爾感測器容錯控制方法 63 4.1 失效偵測方法 63 4.2 錯誤消除方法 68 4.3 容錯控制方法 68 4.4 容錯控制實驗 72 4.4.1 馬達旋轉中單感測器失效 72 4.4.2 馬達靜止下單感測器失效 76 4.4.3 馬達旋轉中雙感測器失效 80 4.4.4 馬達靜止下雙感測器失效 84 4.4.5 馬達旋轉中三感測器失效 88 4.4.6 馬達靜止下三感測器失效 90 4.4.7 容錯實驗總結 92 第5章 結論及未來工作 93 5.1 結論 93 5.1.1 PCB-AFM反應輪馬達設計 93 5.1.2 霍爾感測器冗餘設計及容錯控制 93 5.2 未來工作 94 5.2.1 反應輪設計優化 94 5.2.2 結合混和式角度估測架構 94 參考文獻 96 | - |
| dc.language.iso | zh_TW | - |
| dc.title | 印刷電路板繞組及冗餘位置感測器集成之軸向磁通馬達於衛星反應輪應用 | zh_TW |
| dc.title | Integration of PCB Winding and Redundant Position Sensor in Axial Permanent Magnet Motor for Satellite Reaction Wheel | en |
| dc.type | Thesis | - |
| dc.date.schoolyear | 112-2 | - |
| dc.description.degree | 碩士 | - |
| dc.contributor.oralexamcommittee | 陳景然;陳偉倫;黃仁宏 | zh_TW |
| dc.contributor.oralexamcommittee | Ching-Jan Chen;Woei-Luen Chen;Peter J. Huang | en |
| dc.subject.keyword | 衛星反應輪,霍爾感測器,容錯控制,冗餘設計, | zh_TW |
| dc.subject.keyword | Satellite Reaction Wheel,Hall sensor,Fault tolerant control,Redundant design, | en |
| dc.relation.page | 100 | - |
| dc.identifier.doi | 10.6342/NTU202403553 | - |
| dc.rights.note | 未授權 | - |
| dc.date.accepted | 2024-08-09 | - |
| dc.contributor.author-college | 工學院 | - |
| dc.contributor.author-dept | 機械工程學系 | - |
| 顯示於系所單位： | 機械工程學系 | |
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