المؤلفون: 黃柏徐, Huang, Po-Hsu

المساهمون: 傅立成, Fu, Li-Chen, 臺灣大學:電機工程學研究所

مصطلحات موضوعية: 被動式測距, 順滑模態, 推力向量控制, 側噴流控制系統, 李奧普洛夫定理, Passive ranging, Sliding mode control, Thrust Vector Control, Diver Control System, Lyapunov stability theory, Maneuvering target

وصف الملف: 1027726 bytes; application/pdf

العلاقة: U0001-0808200920531500; http://ntur.lib.ntu.edu.tw/handle/246246/188109Test; http://ntur.lib.ntu.edu.tw/bitstream/246246/188109/1/ntu-98-R96921009-1.pdfTest

الإتاحة: http://ntur.lib.ntu.edu.tw/handle/246246/188109Test
http://ntur.lib.ntu.edu.tw/bitstream/246246/188109/1/ntu-98-R96921009-1.pdfTest

المؤلفون: 薛名雄, Hsueh, Ming-Hsiung

المساهمون: 傅立成, 臺灣大學：電機工程學研究所

مصطلحات موضوعية: 機動目標, 線性可微分賽局, 順滑模態, 推力向量控制, 側噴流控制系統, 李奧普洛夫定理, Linear differential game theory, Sliding mode control, Thrust Vector Control, Diver Control System, Lyapunov stability theory, Maneuvering target

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VanHeeghe, "General 3D guidance law modeling," IEEE International Conference on Systems, Man and Cybernetics, vol. 3, pp. 2013-2018, 1995. [8] E. Duflos, P. Penel, and P. Vanheeghe, "3D guidance law modeling," IEEE Transactions on Aerospace and Electronic Systems, vol. 35, pp. 72-83, 1999. [9] C. Y. Kuo and Y. C. Chiou, "Geometric analysis of missile guidance command," IEE Proc.-Control Theory Appl, vol. 147, pp. 205-211, 2000. [10] C. Y. Kuo, D. Soetanto, and C. Ying-Chwan, "Geometric analysis of flight control command for tactical missile guidance," IEEE Transactions on Control Systems Technology, vol. 9,No.2, pp. 234-243, 2001. [11] C. L. L. a. Y. Y. Chen, "Design of fuzzy logic guidance law against high-speed target," Journal of Guidance, Control, and Dynamics, vol. 23, pp. 17-25, 2000. [12] C. L. Lin, H. Z. Hung, Y. Y. Chen, and B. S. Chen, "Development of an integrated fuzzy-logic-based missile guidance law against high speed target," IEEE Transactions on Fuzzy Systems, vol. 12, pp. 157-169, 2004. [13] S. Gutman, "On optimal guidance for homing missiles," Journal of Guidance and Control, vol. 2, pp. 296–300, 1979. [14] I. Forte and J. Shinar, "Improved guidance law design based on the mixed-strategy concept," Journal of Guidance, Control and Dynamics, vol. 12, pp. 739-745, 1989. [15] D. G. Hull, J. L. Speyer, and D. B. Burris, "Linear-quadratic guidance law for dual control of homing missiles," Journal of Guidance, Control, and Dynamics, vol. 13, pp. 137-144, 1990. [16] S. Josef, M. Guelman, and A. Green, "Game optimal guidance law synthesis for short range missiles," Journal of Guidance, Control, and Dynamics, vol. 15, pp. 191-197, 1992. [17] S. Josef, I. Forte, and B. Kantor, "Mixed Ssrategy guidance: a new high-performance missile guidance law," Journal of Guidance, Control, and Dynamics, vol. 16, pp. 129–135, 1994. [18] S. Josef, "On the feasibility of'hit-to-kill' in the interception of maneuvering targets," Proceedings of American Control Conference, vol. 5, pp. 3358-3363, 2001. [19] T. Vladimir and S. Josef "Missile guidance laws based on pursuit-evasion game formulations," Automatica, vol. 39, pp. 607-618, 2003. [20] S. Josef, T. Vladimir, and O. Yaakov, "Integrated estimation/guidance design approach for improved homing against randomly maneuvering targets " Journal of Guidance, Control, and Dynamics vol. 30, pp. 154-161, 2007. [21] B. Wie, H. Weiss, and A. Arapostathis, "Quaternion feedback regulator for spacecraft eigenaxis rotations," Journal of Guidance, Control, and Dynamics, vol. 12, pp. 375-380, 1989. [22] F. K. Yeh, H. H. Chine, and L. C. Fu, "Nonlinear optimal sliding mode midcourse controller with thrust vector control," Proceedings of the American Control Conference, vol. 2, pp. 1348-1353, 2002. [23] Y. H. OH, "Three dimensional interpolation method for missile aerodynamics," AIAA Aerospace Sciences Meeting, 27th, Reno, NV, 1989. [24] 鄭凱元, "Rocket controller design with TVC and DCS," Department of Electrical Engineering, National Taiwan University, Master Thesis, 2002. [25] 葉富光, "Variable structure theory based integrated guidance/autopilot design for maneuvering flying vehicles," Department of Electrical Engineering, National Taiwan University, Ph.D. Dissertation, 2003. [26] 鄭家豪, "Novel guidance law and autopilot designs for intercepting missiles and launch rockets with TVC and DCS," Department of Electrical Engineering, National Taiwan University, Master Thesis, 2004. [27] 葉俊文, "Adaptive controller design for launch rockets with TVC and DCS," Department of Electrical Engineering, National Taiwan University, Master Thesis, 2005. [28] 林以凡, "Novel control design for intercepting missiles with highly maneuverable autopilot system," Department of Electrical Engineering, National Taiwan University, Master Thesis, 2006. [29] P. Zarchan, "Tactical and Strategic Missile Guidance," American Institute of Aeronautics and Astronautics, Inc, vol. 99, 2002. [30] J. R. Wertz, "Spacecraft Attitude Determination and Control," Kluwer Academic Publishers, 1978. [31] S. Gutman, "Applied min-max approah to missile guidance and control " American Institute of Aeronautics and Astronaustic 2005.; en-US; http://ntur.lib.ntu.edu.tw/handle/246246/53423Test

الإتاحة: http://ntur.lib.ntu.edu.tw/handle/246246/53423Test