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完整後設資料紀錄
DC 欄位 | 值 | 語言 |
---|---|---|
dc.contributor.advisor | 傅立成 | |
dc.contributor.author | Chun-Wen Yeh | en |
dc.contributor.author | 葉俊文 | zh_TW |
dc.date.accessioned | 2021-06-13T07:01:52Z | - |
dc.date.available | 2006-07-28 | |
dc.date.copyright | 2005-07-28 | |
dc.date.issued | 2005 | |
dc.date.submitted | 2005-07-26 | |
dc.identifier.citation | [1] Slotine, J.J.E. and W.Li, Applied Nonlinear Control, Prentice-Hall, 1991.
[2] Hassan K. Khalil, Nonlinear Systems, Prentice-Hall, 2000. [3] Petros A. Ioannou, Robust Adaptive Control, Prentice-Hall, 1996. [4] 陳永平 張浚林,可變結構控制設計,全華, 2002. [5] Peter C. Hughes, Spacecraft Attitude Dynamics, John Wiley & Sons, 1986. [6] 蔡祈旺, “A Nonlinear Missile Guidance Controller with Pulse Type Input devices,” 國立台灣大學電機工程學研究所, Master’s Thesis, 1998. [7] 錢宣浩, “A Midcourse Guidance Law with Thrust Vector Control,” 國立台灣大學電機工程學研究所, Master’s Thesis, 2000. [8] 鄭凱元, “Rocket Controller Design with TVC and DCS,” 國立台灣大學電機工程學研究所, Master’s Thesis, 2002. [9] 葉富光, “Variable Structure Theory Based Integrated Guidance/Autopilot Design for Highly Maneuverable Flying Vehicles,” 國立台灣大學電機工程學研究所, Doctor of Philosophy’s Thesis, 2000. [10] Chia-Hao Cheng, Fu-Kuang Yeh, and Li-Chen Fu, “New Guidance Law and Autopilot Design for Launch Rockets” Accepted by IFAC 2005. [11] George P. Sutton, Rocket Propulsion Elements: An Introduction to the Engineering of Rocket, John Wiley & Sons, Inc., 1992. [12] R. Lioyd, “A Review of Thrust Vector Control Systems for Tactical Missile,” AIAA/SAE Conference, 1978. [13] Gal-Or, Benjamin, “Thrust Vectoring for Flight Control and Safety- A Review,” International Journal of Turbo and Jet-Engines, vol. 11, no. 2-3, p. 119-138, 1994. [14] Emmanuel Duflos, Patrick Penel, Philippe Vanheeghe, “3D guidance Law Modeling”, IEEE transactions on Aerospace and Electrionic System, Vol. 35, No. 1, 1999, pp. 72-83. [15] U. S. Shukla, P. R. Mahapatra, “Generalized Linear Solution of Proportional Navigation”, IEEE Transactions on aerospace and Electrionic systems Vol. 24, No. 3, 1988, pp.231-238. [16] U. S. Shukla, P. R. Mahapatra, “Accurate Soution of Proportional Navigation for Maneuvering Targets”, IEEE Transactions on aerospace and Electrionic systems Vol. SES-25, No. 1, 1989, pp.81-89. [17] Di Zhou, Chundi Mu, Qiang Ling, and Wenli Xu, “Optimal Sliding-Mode Guidance of a Homing-Missile”, Proceedings of the 38th Conference on Decision & Control, 1999, pp. 5131-5136. [18] Chen, Y. P. and S. C. Lo, “Sliding-Mode Controller Design for Spacecraft Attitude Tracking Maneuvers,” IEEE Trans. On Aerospace and Electronic System, vol. 29, no. 4, pp. 1328-1333, 1993. [19] Lo, S. C. and Y. P. Chen, “Smooth Sliding-Mode Control for Spacecraft Attitude Tracking Maneuvers,” Journal of Guidance Control, and Dynamics, vol. 18, no.6, pp. 1345-1349, 1995. [20] J. G. Lee, C. G. Park, and H. W. Park, “Sliding-Mode Controller Design for Spacecraft Attitude Tracking Maneuvers,” IEEE Trans. On aerospace and electronic systems, vol. 29, no. 4, pp. 1328-1333, 1993. [21] Slotine, J. J. E. and M. D. Di Benedetto, “Hamiltonian Adaptive Control of Spacecraft,” IEEE Trans. On automatic control, vol. 35, no. 7, pp. 848-852, 1990. [22] Slotine, J. J. E., “Sliding Controller Design for Nonlinear Systems,” Int. Journal of Control, vol. 40, no. 2, pp. 421-434,1984. [23] B. Castillo Toledo and S. Di Gennaro, “Structurally Stable Attitude Tracking for Rigid Spacecraft with Parameter Uncertainties,” Proceedings of the 41st IEEE Conference on Decision and Control Las Vegas, Nevada USA, December 2002. [24] Slotine, J. J. E. and W. Li, “On the Adaptive Control of Robot Manipulators,” The International Journal of Robotics Research, vol. 6, no. 3, pp. 49-59, 1987. [25] Slotine, J. J. E. and W. Li, “Adaptive Manipulator Control: A Case Study,” IEEE Trans. On automatic control, vol. 33, no. 11, pp. 995-1003, 1988. [26] P. E. Crouch, “Spacecraft attitude control and stabilization: applications of geometric control theory to rigid body models,” IEEE Trans. Automatic control, vol. 29, no. 4, pp. 321-331, 1984. [27] Taiwan’s National Space Program Office, http://www.nspo.gov.tw | |
dc.identifier.uri | http://tdr.lib.ntu.edu.tw/jspui/handle/123456789/35627 | - |
dc.description.abstract | 論文針對具推力向量控制(TVC)及側噴流系統(DCS)的運載火箭,在參數未知下,提出具強健自動駕駛儀之適應控制系統設計。此適應控制器包含了導引律及自動駕駛儀兩部份。為了因應自動駕駛儀造成的姿態誤差,我們也提出解決方法,最後利用巴氏的引理(Barbalat’s Lemma) 證明,確實訊號最後收斂。
在實際模擬中,我們進一步發現,雖然我們理論證實所提出的適應控制法則正確,但由於為積分形式,模擬會造成誤差的累積,進而影響到結果非預期,我們也另外提出適應控制修正方法,並且利用輸入-狀態穩定原理(Input-to-State Stability),證明系統穩定,且訊號收斂到有限範圍內。並以模擬加以佐證可行性,模擬中包含了空氣動力學模型。 最後,要特別強調,我們由實驗中發現,當質量瞬間變化過大時,我們所提出的適應控制法則會無法達到預期目標,也就是我們提出的適應控制法則只適用於質量瞬間變化不大的前提下,才能達成我們的目標,這與我們提出的假設相當符合。 | zh_TW |
dc.description.provenance | Made available in DSpace on 2021-06-13T07:01:52Z (GMT). No. of bitstreams: 1 ntu-94-R88921102-1.pdf: 728115 bytes, checksum: 52d044a4d1ef8f55a277d16b04a60a04 (MD5) Previous issue date: 2005 | en |
dc.description.tableofcontents | 1 序論---------------------------------------------1
1.1 研究動機……………………………………………………1 1.2 相關文獻的回顧……………………………………………2 1.3 論文貢獻……………………………………………………2 1.4 論文組織……………………………………………………3 2 基本知識-----------------------------------------4 2.1 火箭之數學模型……………………………………………4 2.2 四元數數學概念……………………………………………5 2.3 順滑模式概念………………………………………………8 2.4 推力向量控制和側噴流系統………………………………11 2.5 問題描述……………………………………………………13 3 未考慮曲率中心之控制器設計……………………………14 3.1 追蹤軌跡之導引律控制器設計……………………………14 3.2 自動駕駛儀之控制器設計…………………………………18 3.3 自動駕駛儀姿態誤差分析…………………………………22 3.4 導引律控制法則修正………………………………………25 3.5 整合導引律與自動駕駛儀穩定分析………………………27 4 未考慮曲率中心之適應控制器設計------------------29 4.1 導引律適應控制器設計……………………………………29 4.2 自動駕駛儀之適應控制器設計……………………………34 4.3 導引律適應控制法則修正…………………………………39 4.4 整合導引律與自動駕駛儀穩定分析………………………44 5 考慮曲率中心之控制器設計………………………………47 5.1 導引律適應控制器設計……………………………………47 5.2 自動駕駛儀姿態誤差分析…………………………………51 5.3 導引律適應控制法則修正…………………………………54 5.4 整合導引律與自動駕駛儀穩定分析………………………56 6 考慮曲率中心之適應控制器設計…………………………58 6.1 導引律適應控制器設計……………………………………58 6.2 導引律適應控制法則修正…………………………………63 6.3 整合導引律與自動駕駛儀穩定分析………………………68 7 火箭整合系統之模擬………………………………………70 7.1 未考慮曲率中心之模擬……………………………………70 7.2 考慮曲率中心之模擬………………………………………75 8 結論…………………………………………………………………80 參考文獻……………………………………………………………82 | |
dc.language.iso | zh-TW | |
dc.title | 具推力向量及側噴流系統之運載火箭適應控制器設計 | zh_TW |
dc.type | Thesis | |
dc.date.schoolyear | 93-2 | |
dc.description.degree | 碩士 | |
dc.contributor.oralexamcommittee | 馮蟻剛,簡江儒,練光祐 | |
dc.subject.keyword | 運載火箭適應控制器設計, | zh_TW |
dc.subject.keyword | Adaptive Controller Design for Launch Rockets, | en |
dc.relation.page | 84 | |
dc.rights.note | 有償授權 | |
dc.date.accepted | 2005-07-27 | |
dc.contributor.author-college | 電機資訊學院 | zh_TW |
dc.contributor.author-dept | 電機工程學研究所 | zh_TW |
顯示於系所單位: | 電機工程學系 |
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