留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

空间电动力绳系统理论及实验研究

余本嵩,文浩,金栋平,陈提

downloadPDF
余本嵩, 文浩, 金栋平, 陈提. 空间电动力绳系统理论及实验研究[J]. 力学进展, 2016, 46(1): 201605. doi: 10.6052/1000-0992-15-029
引用本文: 余本嵩, 文浩, 金栋平, 陈提. 空间电动力绳系统理论及实验研究[J]. 力学进展, 2016, 46(1): 201605.doi:10.6052/1000-0992-15-029
YU Bensong, WEN Hao, JIN Dongpingy, CHEN Ti. Theory and experiment of space electrodynamic tether systems[J]. Advances in Mechanics, 2016, 46(1): 201605. doi: 10.6052/1000-0992-15-029
Citation: YU Bensong, WEN Hao, JIN Dongpingy, CHEN Ti. Theory and experiment of space electrodynamic tether systems[J].Advances in Mechanics, 2016, 46(1): 201605.doi:10.6052/1000-0992-15-029

空间电动力绳系统理论及实验研究

doi:10.6052/1000-0992-15-029
基金项目:国家自然科学基金(11202094,11290153)、机械结构力学及控制国家重点实验室自主课题(0113Y01)及江苏高校优势学科建设工程资助项目.
详细信息
    作者简介:

    金栋平,博士,教授,博士生导师.南京航空航天大学机械结构力学及控制国家重点实验室副主任、结构工程与力学系主任.科学出版社《非线性动力学丛书》《Acta Mechanica Sinica》《航空学报》《振动工程学报》《中国科学》等编委.主要从事非线性动力学与控制研究,曾获2005年度国家科技进步奖二等奖和2006年度国家自然科学奖二等奖.

    通讯作者:

    金栋平

  • 中图分类号:V412.4

Theory and experiment of space electrodynamic tether systems

More Information
    Corresponding author:JIN Dongpingy
  • 摘要:本文关注在轨航天器中具有导电性能的电动力绳系统,因其复杂动响应特征及潜在应用前景值得学者们深入研究.论文阐述了电动力绳系统的工作原理,对系统的力学建模、动力学行为、控制、应用、在轨实验及地面实验方法等研究进展进行了详细总结,同时提出电动力绳系统有待进一步探究的科学与技术问题.

  • [1] 蔡洪, 杨育伟, 郭才发. 2014. 电动力绳系研究进展. 宇航学报, 35:1223-1232(Cai H, Yang Y W, Guo C F. 2014. Review of electrodynamic tether system. Journal of Astronautics, 35:1223-1232).
    [2] 陈辉, 文浩, 金栋平, 胡海岩. 2013. 绳系卫星在轨试验及地面物理仿真进展. 力学进展, 43:174-184(Chen H, Wen H, Jin D P, Hu H Y. 2013. Experimental studies on tethered satellite systems. Advances in Mechanics, 43:174-184).
    [3] 孔宪仁, 徐大富. 2010. 空间绳系研究综述. 航天器环境工程, 27:775-783(Kong X R, Xu D F. 2010.The studied of space tether. Spacecraft Environment Engineering, 27:775-783).
    [4] 李然, 许滨, 张珩. 2008. 空间电动绳系推进中导电系绳动态特性分析. 振动与冲击, 27:36-40, 185, 186(Li R, Xu B, Zhang H. 2008. Dynamic feature analysis of space electrodynamic tether systems. Journal of Vibration and Shock, 27:36-40, 185, 186).
    [5] 刘丽丽. 2008. 绳系卫星动力学分析与控制的若干研究.[博士论文]. 南京:南京航空航天大学(Liu L L. 2008. Studies on dynamic analysis and control of tethered satellite systems.[PhD Thesis]. Nanjing:Nanjing University of Aeronautics and Astronautics).
    [6] 刘丽丽, 文浩, 金栋平, 胡海岩. 2011. 三维电动力绳系子卫星轨道转移的最优控制. 计算力学学报, 28:178-182(Liu L L, Wen H, Jin D P, Hu H Y. 2011. Three-dimensional optimal control of orbit transfer for an electrodynamic tethered subsatellite. Chinese Journal of Computational Mechanics, 28:178-182).
    [7] 潘冠群, 许滨, 张珩. 2007. 空间电动绳系推进的动力学建模与分析. 力学与实践, 29:17-22(Pan G Q, Xu B, Zhang H. 2007. Modelling and motion analysis of space electrodynamic tethered systems.Mechanics in Engineering, 29:17-22).
    [8] 潘伟, 路长厚, 李吉栋, 孔令敏. 2011. 基于傅里叶展开的电动力绳系卫星最优控制. 航空学报, 32:1714-1721(Pan W, Lu C H, Li J D, Kong L M. 2011. Optimal control of electrodynamic tethered satellites based on fourier series expansion. Acta Aeronautica et Astronautica Sinica, 32:1714-1721).
    [9] 文浩. 2009. 绳系卫星释放和回收的动力学控制.[博士论文]. 南京:南京航空航天大学(Wen H. 2009.Dynamic control for deployment and retrieval of tethered satellite systems.[PhD Thesis]. Nanjing:Nanjing University of Aeronautics and Astronautics).
    [10] 文浩, 金栋平, 胡海岩. 2008. 倾斜轨道电动力绳系卫星回收控制. 力学学报, 40:375-380(Wen H, Jin D P, Hu H Y. 2008. Retrieval control of an electro-dynamic tethered satellite in an inclined orbit. Chinese Journal of Theoretical and Applied Mechanics, 40:375-380).
    [11] 徐大富. 2010. 电动力绳系离轨系统的建模与动力学分析.[博士论文]. 哈尔滨:哈尔滨工业大学(Xu D F. 2010. Modeling and dynamic analysis of electrodynamic tether deorbiting system.[PhD Thesis]. Harbin:Harbin Institute of Technology).
    [12] 徐大富, 孔宪仁, 刘文佳, 罗文波. 2007. 基于电动力缆绳的卫星离轨时间预测. 吉林大学学报(工学版), 37:1476-1480(Xu D F, Kong X R, Liu W J, Luo W B. 2007. Application of electro-dynamic tether for deorbiting and deorbit time forecast. Journal of Jilin University(Engineering and Technology Edition), 37:1476-1480).
    [13] 余本嵩. 2011. 复杂太空环境下柔性绳系卫星动力学与控制.[博士论文]. 南京:南京航空航天大学(Yu B S. 2011. Dynamic and control of flexible tethered satellite in complex space environment.[PhD Thesis]. Nanjing:Nanjing University of Aeronautics and Astronautics).
    [14] 翟光, 苏飞, 张景瑞, 张尧. 2015. 考虑面内外摆角对电动绳系离轨过程的参数影响分析. 系统工程与电子技术, 37:1837-1843(Zhai G, Su F, Zhang J R, Zhang Y. 2015. Analysis of libration impact on the deorbit mission of space electro-dynamic tether. Systems Engineering and Electronics, 37:1837-1843).
    [15] Agüero V M, Gilchrist B E, Williams S D, Burke W J, Krause L, Gentile L C. 2000. Current collection model characterizing shuttle charging during the tethered satellite system missions. Journal of Spacecraft and Rockets, 37:212-217.
    [16] Andrews J G, Allen J E. 1971. Theory of a double sheath between two plasmas. Proceedings of the Royal Society of London, 320:459-472.
    [17] Aslanov V, Yudintsev V. 2013. Dynamics of large space debris removal using tethered space tug. Acta Astronautica, 91:149-156.
    [18] Banerjee A, Singhose W, Blackburn D. 2005. Orbit boosting of an electrodynamic tethered satellite with input-shaped current. In:Proceedings of AAS/AIAA Astrodynamics Specialist Conference, Lake Tahoe, USA.
    [19] Banks P M, Williamson P R, Oyama K I. 1981. Electrical behavior of a shuttle electrodynamic tether system(SETS). Planetary and Space Science, 29:139-147.
    [20] Bell I C, Hagen K A, Singh V, McCarty S L, Cutler J W, Gilchrist B E, McTernan J K, Bilen S G. 2013. Investigating miniature electrodynamic tethers and interaction with the low earth orbit plasma. In:Proceedings of AIAA Space 2013 Conference and Exposition, San Diego, USA.
    [21] Bilitza D, Reinisch B W. 2008. International Reference Ionosphere 2007:Improvements and new parameters.Advances in Space Research, 42:599-609.
    [22] Bombardelli C. 2012. Power density of a bare electrodynamic tether generator. Journal of Propulsion and Power, 28:664-668.
    [23] Bombardelli C, Zanutto D, Lorenzini E C. 2013. Deorbiting performance of bare electrodynamic tethers in inclined orbits. Journal of Guidance, Control, and Dynamics, 36:1550-1555.
    [24] Bonometti J A, Sorensen K F, Dankanich J W, Frame K L. 2006. 2006 Status of the momentum exchange electrodynamic re-boost(MXER) tether development. In:Proceedings of 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Sacramento, USA.
    [25] Bruno C, Bussolino L, Iess L, Licata R, Schirone L. 2001. EDOARD:a tether device for efficient electrody-namic de-orbiting of LEO spacecraft. In:Proceedings of Space Technology and Applications International Forum, Albuquerque, USA.
    [26] Carroll J A, Oldson J C. 1995. Tethers for small satellite applications. In:Proceedings of AIAA/USU Small Satellite Conference, Logan, USA.
    [27] Cartmell M P, McKenzie D J. 2008. A review of space tether research. Progress in Aerospace Sciences, 44:1-21.
    [28] Choinière É. 2004. Theory and experimental evaluation of a consistent steady-state kinetic model for two-dimensional conductive structures in ionospheric plasmas with application to bare electrodynamic tethers in space.[PhD Thesis]. Michigan:University of Michigan.
    [29] CosmoML, Lorenzini E C. 1997. Tethers in space handbook(3rd ed). Washington DC:National Aeronautics and Space Administration.
    [30] Danilov V V, Elgin B A, Grafodatsky O S, Mirnov V V. 2000. High-voltage satellite tethers for active experiments in space. In:Proceedings of 6th Spacecraft Charging Technology Conference, Huntsville, USA.
    [31] Davis J. 2004. Mathematical modeling of Earth's magnetic field.[Technical Note]. Blacksburg:Virginia Polytechnic Institute and State University.
    [32] Dobrowolny M, Stone N H. 1994. A technical overview of TSS-1:the first tethered-satellite system mission.Il Nuovo Cimento, 17C:1-12.
    [33] Ellis J R, Hall C D. 2009. Model development and code verification for simulation of electrodynamic tether system. Journal of Guidance, Control, and Dynamics, 32:1713-1722.
    [34] Estes R D, Lorenzini E C, Santangelo A. 2000a. An overview of electrodynamic tethers. In:Proceedings of 38th Aerospace Sciences Meeting and Exhibit, Reno, USA.
    [35] Estes R D, Lorenzini E C, Sanmartín J R, Peláez J, Martínez-Sánchez M, Johnson C L, Vas I E. 2000b.Bare tethers for electrodynamic spacecraft propulsion. Journal of Spacecraft and Rockets, 37:205-211.
    [36] Estes R D, Sanmartín J R, Martínez-Sánchez M. 2000c. Performance of bare-tether systems under varying magnetic and plasma conditions. Journal of Spacecraft and Rockets, 37:197-204.
    [37] Forward R L, Hoyt R P, Uphoff C. 1998. Application of the terminator tetherTM electrodynamic drag technology to the deorbit of constellation spacecraft. In:Proceedings of 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, USA.
    [38] Fuhrhop K R P. 2007. Theory and experimental evaluation of electrodynamic tether systems and related technologies.[PhD Thesis]. Michigan:University of Michigan.
    [39] Fuhrhop K R P, West B, Choinière É. 2004. Current collection to electrodynamic-tether systems in space.In:Proceedings of 2nd International Energy Conversion Engineering Conference, Providence, USA.
    [40] Fujii H A, Watanabe T, Sahara H, Kojima H, Takehara S, Yamagiwa Y, Sasaki S, Abe T, Tanaka K, Oyama K, Johnson L, Khazanov V, Sanmartin J R, Charro M, Kruijff M, van der Heide E J, Rubin B, Garcia de Quiros F J, Trivailo P M, Williams P. 2011. Space demonstration of bare electrodynamic tape-tether technology on the sounding rocket S520-25. In:Proceedings of AIAA Guidance, Navigation, and Control Conference, Portland, USA.
    [41] Hoyt R P. 2002. Stabilization of electrodynamic tethers. In:Proceedings of 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, USA.
    [42] Hoyt R P, Minor B M. 2005. Remediation of radiation belts using electrostatic tether structures. In:Proceedings of Aerospace Conference, Piscataway, USA.
    [43] Iki K, Kawamoto S, Morino Y. 2012. Numerical simulations of an electrodynamic tether deployment from a spool-type using thrusters. In:Proceedings of 1st International Academy of Astronautics Conference, San Diego, USA.
    [44] Iki K, Kawamoto S, Morino Y. 2014. Experiments and numerical simulations of an electrodynamic tether deployment from a spool-type reel using thrusters. Acta Astronautica, 94:318-327.
    [45] Iñarrea M, Lanchares V, Pascual A I, Salas J P. 2014. Attitude stabilization of electrodynamic tethers in elliptic orbits by time-delay feedback control. Acta Astronautica, 96:280-295.
    [46] Iñarrea M, Peláez J. 2010. Libration control of electrodynamic tethers using the extended time-delayed autosynchronization method. Journal of Guidance, Control, and Dynamics, 33:923-933.
    [47] Ishige Y, Kawamoto S, Kibe S. 2004. Study on electrodynamic tether system for space debris removal. Acta Astronautica, 55:917-929.
    [48] Janeski J A, Hall C D, Scales W A. 2015. Effects of local plasma environment on dynamics of electrodynamic tether systems. Journal of Spacecraft and Rockets, 52:496-505.
    [49] Johnson L, Carroll J, Estes R D, Lorenzini E C, Gilchrist B, Martinez-Sanchez M, Sanmartin J, Vas I. 1996. Electrodynamic tethers for reboost of the international space station and spacecraft propulsion. In:Proceedings of Space Programs and Technologies Conference, Huntsville, USA.
    [50] Johnson L, Estes R D, Lorenzini E C, Martinez-Sanchez M, Sanmartin J, Vas I. 1998a. Electrodynamic tethers for spacecraft propulsion. In:Proceedings of 36th Aerospace Sciences Meeting and Exhibit, Reno, USA.
    [51] Johnson L, Herrmann M. 1998b. International space station electrodynamic tether reboost study.[Report]. Washington D.C:National Aeronautics and Space Administration, 1998-208538.
    [52] Katz I, Anderson J R, Polk J E, Brophy J R. 2003. One-dimensional hollow cathode model. Journal of Propulsion and Power, 19:595-600.
    [53] Kawamoto S, Makida T, Sasaki F, Okawa Y, Nishida S. 2006. Precise numerical simulations of electrody-namic tethers for an active debris removal system. Acta Astronautica, 59:136-148.
    [54] Kawashima N, Sasaki S, Oyama K I, Hirao K, Obayashi T, Raitt W J, White A B, Williamson P R, Banks P M. 1988. Results from a tethered rocket experiment(Charge-2). Advances in Space Research, 8:197-201.
    [55] Khazanov G V, Krivorutsky E N, Johnson L. 2006. Electrodynamic tether as a thruster for LEO mission ap-plications. In:Proceedings of 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Sacramento, USA.
    [56] Kim I, Hirayama H, Hanada T. 2010. Practical guidelines for electro-dynamic tethers to survive from orbital debris impacts. Advances in Space Research, 45:1292-1300.
    [57] Kojima H, Iwashima H, Trivailo P M. 2011. Libration synchronization control of clustered electrodynamic tether system using kuramoto model. Journal of Guidance, Control, and Dynamics, 34:706-718.
    [58] Kojima H, Sugimoto T. 2007. Nonlinear control of a double pendulum electrodynamic tether system. Journal of Spacecraft and Rockets, 44:280-284.
    [59] Kojima H, Sugimoto T. 2009. Stability analysis of in-plane and out-of-plane periodic motions of electrody-namic tether system in inclined elliptic orbit. Acta Astronautica, 65:477-488.
    [60] Kojima H, Sugimoto T. 2010. Switching delayed feedback control for an electrodynamic tether system in an inclined elliptic orbit. Acta Astronautica, 66:1072-1080.
    [61] Korepanov V, Dudkin F. 2001. Electrodynamic tether system-possibility of realisation. Physics and Chem-istry of the Earth, 26:281-283.
    [62] Lanoix E L M, Misra A K, Modi V J, Tyc G. 2005. Effect of electrodynamic forces on the orbital dynamics of tethered satellites. Journal of Guidance, Control, and Dynamics, 28:1309-1315.
    [63] Larsen M B, Blanke M. 2007. Nonlinear control of electrodynamic tether in equatorial or somewhat inclined orbits. In:Proceedings of 15th Mediterranean Conference on Control and Automationt, Athens, Greece.
    [64] Larsen M B, Blanke M. 2009. Control by damping injection of electrodynamic tether system in an inclined orbit. In:Proceedings of 2009 American Control Conference, St. Louis, USA.
    [65] Mankala K K, Agrawal S K. 2005. Equilibrium-to-equilibrium maneuvers of rigid electrodynamic tethers.Journal of Guidance, Control, and Dynamics, 28:541-545.
    [66] Mankala K K, Agrawal S K. 2006. Equilibrium-to-equilibrium maneuvers of flexible electrodynamic tethers in equatorial orbits. Journal of Spacecraft and Rockets, 43:651-658.
    [67] Mantellato R, Pertile M, Colombatti G, Lorenzini E C. 2013. Analysis of passive system to damp the libration of electrodynamic tethers for deorbiting. In:Proceedings of AIAA SPACE 2013 Conference and Exposition, San Diego, USA.
    [68] Marshall L S, Griger R V. 1995. Deployer performance results for the TSS-1 mission.[Report]. Washington DC:National Aeronautics and Space Administration, NASA-CR-202595.
    [69] McTernan J K, Bilén S G. 2013. The plasma-spacecraft interface on small-scale spacecraft with implications for electrodynamic tether systems. In:Proceedings of AIAA Space 2013 Conference and Exposition, San Diego, USA.
    [70] Morris D. 2005. Optimizing space-charge limits of electron emission into plasmas in space electric propulsion.[PhD Thesis]. Michigan:University of Michigan.
    [71] Ohkawa Y, Kitamura S, Kawamoto S, Matsumoto K, Kibe S, Matsumoto T, Murata F, Matsui M, Yamagiwa Y. 2011. A carbon nanotube field emission cathode for electrodynamic tether systems. In:Proceedings of 32nd International Electric Propulsion Conference, Wiesbaden, Germany.
    [72] Oishi A, Hirayama H, Hanada T, Yasaka T, Pardini C, Anselmo L. 2004. Assessment of collision risk to electrodynamic tether used for de-orbiting. In:Proceedings of 55th International Astronautical Congress, Vancouver, Canada.
    [73] Okawa Y, Kitamura S, Kawamoto S. 2007. An experimental study on carbon nanotube cathodes for elec-trodynamic tether propulsion. Acta Astronautica, 61:989-994.
    [74] Pardini C, Hanada T, Krisko P H. 2009. Benefits and risks of using electrodynamic tethers to de-orbit spacecraft. Acta Astronautica, 64:571-588.
    [75] Pardini C, Hanada T, Krisko P H, Anselmo L, Hirayama H. 2007. Are de-orbiting missions possible using electrodynamic tethers? Task review from the space debris perspective. Acta Astronautica, 60:916-929.
    [76] Pearson J. 2010. The electrodynamic debris eliminator(EDDE) removing debris in space. The Bent of Tau Beta Pi, spring:17-21.
    [77] Pearson J, Carroll J, Levin E, Oldson J, Hausgen P. 2003. Overview of the electrodynamic delivery express(EDDE). In:Proceedings of 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA.
    [78] Pearson J, Levin E, Carroll J A, Oldson J C. 2004. Orbital maneuvering with spinning electrodynamic tethers. In:Proceedings of 2nd International Energy Conversion Engineering Conference, Providence, USA.
    [79] Peláez J, Andrés Y N. 2005a. Dynamic stability of electrodynamic tethers in inclined elliptical orbits.Journal of Guidance, Control, and Dynamics, 28:611-622.
    [80] Peláez J, Lorenzini E C. 2005b. Libration control of electrodynamic tethers in inclined orbit. Journal of Guidance, Control, and Dynamics, 28:269-278.
    [81] Peláez J, Lara M. 2003. Periodic solutions in electrodynamic tethers on inclined orbits. Journal of Guidance, Control, and Dynamics, 26:395-406.
    [82] Peláez J, Lorenzini E C, Lopez-Rebollal O, Ruiz M. 2000. A new kind of instability of electrodynamic tethers. In:Proceedings of AAS/AIAA Space Flight Mechanics Meeting, Clearwater, USA.
    [83] Peláez J, Ruiz M, López-Rebollal O, Lorenzini E C, Cosmo M L. 2002. Two-bar model for the dynamics and stability of electrodynamic tethers. Journal of Guidance, Control, and Dynamics, 25:1125-1135.
    [84] Peláez J, Sanjurjo M. 2006a. Generator regime of self-balanced electrodynamic bare tethers. Journal of Spacecraft and Rockets, 43:1359-1369.
    [85] Peláez J, Sanjurjo M. 2006b. Self-balanced electrodynamic tehters for space debris mitigation. In:Proceed-ings of 57th International Astronautical Congress, Valencia, Spain.
    [86] Peláez J, Sanjurjo M, Fontdecabe J. 2004. Satellite deorbiting using a self balanced electrodynamic tether.In:Proceedings of 55th International Astronautical Congress, Vancouver, Canada.
    [87] Rasmussen C E, Banks P M. 1988. Theory of the electrodynamic tether. Advances in Space Research, 8:203-211.
    [88] Robertson M J. 2005. Command generation and control of momentum exchange electrodynamic reboost tethered satellite.[Final Report of Graduate Student Researchers Program]. Washington D.C:National Aeronautics and Space Administration.
    [89] Sabey N, Tragesser S. 2008. Effects of libration on general electrodynamic tether orbital maneuvers. In:Proceedings of AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Honolulu, USA.
    [90] Samanta Roy R I, Hastings D E, Ahedo E. 1992. Systems analysis of electrodynamics tethers. Journal of Spacecraft and Rockets, 29:415-424.
    [91] San H. 2002. Orbital maneuvering using electrodynamic tethers.[Master Thesis]. Dayton:Air Force Institute of Technology.
    [92] Sánchez-Arriaga G, Bombardelli C, Chen X. 2015. Impact of nonideal effects on bare electrodynamic tether performance. Journal of Propulsion and Power, 31:951-955.
    [93] Sanjurjo-Rivo M. 2009. Self balanced bare electrodynamic tethers. Space debris mitigation and other applications.[PhD Thesis]. Madrid:Universidad Politécnica de Madrid.
    [94] Sanjurjo-Rivo M, Peláez J. 2011. Energy analysis of bare electrodynamic tethers. Journal of Propulsion and Power, 27:246-256.
    [95] Sanjurjo-Rivo M, Scheeres D J, Peláez J. 2014. Jovian capture of a spacecraft with a self-balanced electro-dynamic bare tether. Journal of Spacecraft and Rockets, 51:1401-1412.
    [96] Sanmartín J R. 2010a. A review of electrodynamic tethers for science applications. Plasma Source Science and Technology, 19:34022-34028.
    [97] Sanmartín J R, Lorenzini E C, Martinez-Sanchez M. 2010b. Electrodynamic tether applications and con-straints. Journal of Spacecraft and Rockets, 47:442-456.
    [98] Sanmartín J R, Charro M. 2006a. Performance of electrodynamic tethers and ion thrusters against hybrid systems. Journal of Propulsion and Power, 22:698-700.
    [99] Sanmartín J R, Elaskar S A. 2006b. Efficiency of electrodynamic tether thrusters. Journal of Spacecraft and Rockets, 43:659-666.
    [100] Sanmartín J R, Lorenzini E C. 2005. Exploration of outer planets using tethers for power and propulsion.Journal of Propulsion and Power, 21:573-576.
    [101] Sanmartín J R, Martínez-Sánchez M, Ahedo E. 1993. Bare wire anodes for electrodynamic tethers. Journal of Propulsion and Power, 9:353-360.
    [102] Sasaki S, Oyama K I, Kawashima N, Watanabe Y, Obayashi T, Raitt W J, White A B, Banks P M, Williamson P R, Sharp W F, Yokota T, Hirao K. 1987. Results from a series of tethered rocket experi-ments. Journal of Spacecraft and Rockets, 24:444-453.
    [103] Schadegg M M, Russell R P, Lantoine G. 2015. Jovian orbit capture and eccentricity reduction using electrodynamic tether propulsion. Journal of Spacecraft and Rockets, 52:506-516.
    [104] Sedwick R J, Schweighart S A. 2002. Propellantless spin-up of tethered or electromagnetically coupled sparse apertures. In:Proceedings of SPIE, 4849:193-204.
    [105] Shiah A, Hwang K S, Wu S T, Stone N H. 1997. Three-dimensional simulation of current collection in space.Planetary and Space Science, 45:475-482.
    [106] Stevens R E. 2008a. Optimal control of electrodynamic tether satellites.[PhD Thesis]. Dayton:Air Force Institute of Technology.
    [107] Stevens R E, Wiesel W. 2008b. Large time scale optimal control of an electrodynamic tether satellite.Journal of Guidance, Control, and Dynamics, 31:1716-1727.
    [108] Stevens R E, Baker W P. 2009. Optimal control of a librating electrodynamic tether performing a multirev-olution orbit change. Journal of Guidance, Control, and Dynamics, 32:1497-1507.
    [109] Stone N H. 1996. Electrodynamic characteristics of the tethered satellite system during the TSS-1R mission.In:Proceedings of AIAA Space Programs and Technologies Conference, Huntsville, USA.
    [110] Stone N H, Gierow P A. 2001. A preliminary assessment of passive end-body plasma contactors. In:Proceedings of 39th Aerospace Sciences Meeting and Exhibit, Reno, USA.
    [111] Stone N H, Raitt W J, Wright K H. 1999. The TSS-1R electrodynamic tether experiment:scientific and technological results. Advances in Space Research, 24:1037-1045.
    [112] Tahara H, Nishio H, Onishi T. 2004. Basic study of electron collection by a bare tethered satellite. Vacuum, 73:455-460.
    [113] Takeichi N. 2006. Practical operation strategy for deorbit of an electrodynamic tethered system. Journal of Spacecraft and Rockets, 43:1283-1288.
    [114] Tortora P, Somenzi L, Iess L, Licata R. 2006. Small mission design for testing in-orbit an electrodynamic tether deorbiting system. Journal of Spacecraft and Rockets, 43:883-892.
    [115] Tragesser S G, San H. 2003. Orbital maneuvering with electrodynamic tethers. Journal of Guidance, Control, and Dynamics, 26:805-810.
    [116] Tyc G, Han R P S. 1995. Attitude dynamics investigation of the OEDIPUS-A tethered rocket payload.Journal of Spacecraft and Rockets, 32:133-141.
    [117] Valverde J, Escalona J L, Mayo J, Domínguez J. 2003. Dynamic analysis of a light structure in outer space-short electrodynamic tether. Multibody System Dynamics, 10:125-146.
    [118] Valverde J, van der Heijden G H M. 2010. Magnetically-induced buckling of a whirling conducting rod with applications to electrodynamic space tethers. Journal of Nonlinear Science, 20:309-339.
    [119] van Dijk A, Kruijff M, van der Heide E J, Lebreton J P. 2003. LeBRETON, a lightweight bare rotating tether system for Jovian atmospheric entry. In:Proceedings of 54th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law, Bremen, Germany.
    [120] Vannaroni G, Dobrowolny M, De Venuto F. 2001. Deorbiting with electrodynamic tethers comparison between different tether configurations. Space Debris, 1:159-172.
    [121] Vas I E, Kelly T J, Scarl E A. 2000. Space station reboost with electrodynamic tethers. Journal of Spacecraft and Rockets, 37:154-164.
    [122] Vaughn J A, Curtis L, Gilchrist B E. 2004. Review of the ProSEDS electrodynamic tether mission develop-ment. In:Proceedings of 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, USA.
    [123] Viennet E, Steindl A, Troger H. 2005. Control of electrodynamic tether vibrations in space. Proceedings in Applied Mathematics and Mechanics, 5:141-142.
    [124] Vigneron F R, Schultz F, Jablonski A M, Tyc G. 1998. Tether deployment and trajectory modeling for the OEDIPUS missions. AIAA-98-4553.
    [125] Watanabe T, Makida T, Fujii H A, Kojima H, Singhose W. 2004. An application of input shaping for electrodynamic tether system. In:Proceedings of AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Providence, USA.
    [126] Wen H, Jin D P, Hu H Y. 2008. Advances in dynamics and control of tethered satellite systems. Acta Mechanica Sinica, 24:229-241.
    [127] Williams J D, Sanmartin J R, Rand L P. 2012. Low work-function coating for an entirely propellantless bare electrodynamic tether. IEEE Transactions on Plasma Science, 40:1441-1445.
    [128] Williams P. 2005a. Optimal orbital transfer with electrodynamic tether. Journal of Guidance, Control, and Dynamics, 28:369-372.
    [129] Williams P. 2005b. Optimal orbital maneuvers using electrodynamic tethers. In:Proceedings of AAS/AIAA Astrodynamics Specialist Conference, Lake Tahoe, USA.
    [130] Williams P. 2006a. Periodic solutions of electrodynamic tethers under forced current variations. In:Pro-ceedings of AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Keystone, USA.
    [131] Williams P. 2006b. Simple approach to orbital control using spinning electrodynamic tethers. Journal of Spacecraft and Rockets, 43:253-256.
    [132] Williams P. 2006c. Energy rate feedback for libration control of electrodynamic tethers. Journal of Guidance, Control, and Dynamics, 29:221-223.
    [133] Williams P. 2009. Libration control of electrodynamic tethers using predictive control with time-delayed feedback. Journal of Guidance, Control, and Dynamics, 32:1254-1268.
    [134] Williams P. 2010. Optimal control of electrodynamic tether orbit transfers using timescale separation.Journal of Guidance, Control, and Dynamics, 33:88-98.
    [135] Williams S D. 1999. Using an electrodynamic tethered satellite as anionospheric electric double probe to estimate tethered satellite motion and measure vertical electric field.[PhD Thesis]. Ann Arbor:Stanford University.
    [136] Yamaigiwa Y, Hiragi E, Kishimoto T. 2005. Dynamic behavior of electrodynamic tether deorbit system on elliptical orbit and its control by Lorentz force. Aerospace Science and Technology, 9:366-373.
    [137] Yu B S, Wen H, Jin D P. 2015. A new stabilization strategy for deployment of tethered satellite systems in three-dimensional space. Acta Mechanica(under review)
    [138] Zakrzhevslii A E, Pirozhenko A V. 2007. Motion parameters of an electrodynamic tether in orbit. Interna-tional Applied Mechanics, 43:335-343.
    [139] Zanutto D, Curreli D, Lorenzini E C. 2011. Stability of electrodynamic tethers in a three-body system.Journal of Guidance, Control, and Dynamics, 34:1441-1456.
    [140] Zeineh C F. 2005. Applications of an electrostatic high-voltage tether to radiation belt remediation.[Master Thesis]. Cambridge:Massachusetts Institute of Technology.
    [141] Zhong R, Zhu Z H. 2012. Dynamics of deorbiting of low earth orbit nano-satellites by bare electrodynamic tether. In:Proceedings of AIAA SPACE 2012 Conference and Exposition, Pasadena, USA.
    [142] Zhong R, Zhu Z H. 2013a. Dynamics of nanosatellite deorbit by bare electrodynamic tether in low earth orbit. Journal of Spacecraft and Rockets, 50:691-700.
    [143] Zhong R, Zhu Z H. 2013b. Nano-satellite deorbit by bare electrodynamic tether. In:Proceedings of AIAA Atmospheric Flight Mechanics Conference, Boston, USA.
    [144] Zhong R, Zhu Z H. 2013c. Libration dynamics and stability of electrodynamic tethers in satellite deorbit.Celestial Mechanics and Dynamical Astronomy, 116:279-298.
    [145] Zhong R, Zhu Z H. 2013d. Long term dynamics and optimal control of nano-satellite deorbit using a short electrodynamic tether. Advances in Space Research, 52:1530-1544.
    [146] Zhong R, Zhu Z H. 2013e. Hybrid optimal control based on current on-off regulation of a short electrodynamic tether. In:Proceedings of AIAA Space 2013 Conference and Expossition, San Diego, USA.
    [147] Zhong R, Zhu Z H. 2014. Optimal control of nanosatellite fast deorbit using electrodynamic tether. Journal of Guidance, Control, and Dynamics, 37:1182-1193.
    [148] Zhou X, Li J F, Baoyin H X, Zakirov V. 2006. Equilibrium control of electrodynamic tethered satellite systems in inclined orbits. Journal of Guidance, Control, and Dynamics, 29:1451-1454.
    [149] Zhu Z H, Zhong R. 2011. Deorbiting dynamics of electrodynamic tether. International Journal of Aerospace and Lightweight Structures, 1:47-66.
  • 加载中
计量
  • 文章访问数:2188
  • HTML全文浏览量:260
  • PDF下载量:2375
  • 被引次数:0
出版历程
  • 收稿日期:2015-06-18
  • 修回日期:2015-09-14
  • 刊出日期:2016-05-20

目录

    /

      返回文章
      返回

        Baidu
        map