-
摘要:
通过系绳释放、运行和回收的在轨卫星称为绳系卫星. 绳系卫星功能独特, 在人工重力梯度、空间传送、电动力推进等方面应用广泛. 本文以绳系卫星为对象, 概述了全世界历年来绳系卫星的在轨飞行试验, 包括试验背景、目的、步骤以及结果等; 介绍了近年来绳系卫星的地面物理仿真实验技术, 分析了系统结构、仿真原理以及实验结果; 对未来我国空间绳系卫星技术的发展提出建议.
Abstract:The tethered satellite system, which is deployed from another ying vehicle in space via a tether, is a new technology for arti cial gravity creation, LEO to GEO tether transportation, scientific and technological applications, electro-dynamic study, and so on. This paper first surveys experimental researches of the tethered satellite systems on orbit, including the mission backgrounds, motivations, manipulate procedures and relevant experimental results. Then it reviews the con guration of ground-based experiments, covering both the equivalent principium and the experimental results. Finally, the paper addresses some open problems related to the tethered satellite technology to be developed in China.
-
1 Schultz F W, Vigneron F R, Jablonski A M. Horizontallyconfigured ground-test method for tethered satellites. Canadian Aeronautics and Space Journal, 2002, 48(1):97-106 2 Vigneron F R, Schultz F, Jablonski A M, et al. Tether deployment and trajectory modeling for space plasma science missions. Journal of Spacecraft and Rockets, 2000,37(1): 78-85 3 Lansdorp B, Soemers I H M J, Van Der Heide E J, et al. Design of a high-tension elastically deforming space tether deployer. In: 55th International Astronautical Congress. Vancouver, Canada, 2004. 1-6 4 Menon C, Kruijff M, Vavouliotis A, et al. A European barberpole mechanism for space tether deployment. In: AIAA, 56th International Astronautical Congress, Fukuoka, Japan, 2005 5 Chang C L, Drobot A T, Papadopoulos K, et al. Currentvoltage characteristics of the tethered satellite system: Measurements and uncertainties due to temperature variations. Geophysical Research Letters, 1998, 25(5): 713-716 6 Sorensen K F. Conceptual design and analysis of an MXER tether boost station. AIAA3915, 2001 7 Forward R L, Hoyt R P, Uphoff C W. Terminator tether: a spacecraft deorbit device. Journal of Spacecraft and Rockets, 2000, 37(2): 187-196 8 Cosmo M L, Lorenzini E C. Tether in space handbook. Huntsville, AL: Smithsonian Astrophysical Observatory, NASA Marshall Space Flight Center, 1997 9 Dobrowolny M, Stone N H. A technical overview of TSSI: the first tethered-satellite system mission. Nuovo CimentoSocieta Italiana di Fisica Sezione C, 1994,17(1): 1-12 10 Carroll J A, Oldson J C. Tethers for small satellite applications. In: AIAA/USU Small Satellite Conference, Logan, Utah, 1995 11 Mccoy J E, C. O'Neill J S, Settecerri T, et al. Plasma motor-generator (PMG) flight experiment results. In: Proceedings of the 4th International conference on Tethers in Space, Washington DC, 1995. 12 Kramer H J. Observation of the Earth and its Environment. Berlin, Heidelberg: Springer Verlag, 2002 13 Laframboise J G, Wallis D D, James H G. Effects of largeamplitude RF emissions on OEDIPUS-C floating voltages. In: 8th Spacecraft Charging Technology Conference, English,2004 14 Johnson L, Ballance J. Propulsive small expendable deployer system (ProSEDS) space demonstration. Space Technology and Applications. Albuquerque, 1998 15 Kawashima N, Sasaki S, Oyama K I, et al. Results from a tethered rocket experiment (Charge-2). Advances in Space Research, 1988, 8(1): 197-201 16 James P. Hypervelocity impact studies on space tethers. In: 54th International Astronautical Congress of the International Astronautical Federation (IAF). Bremen, Germany,2003 17 Koss S. Tether Deployment mechanism for the advanced tether experiment (ATEx). In: Proceeding 7th European Space Mechanisms & Tribology Symposium. ESTEC, Noordwijk, The Netherlands, 1997. 175-182 18 Kruijff M, Vanderheide E. Qualification and in-flight demonstration of a european tether deployment system on YES2. Acta Astronautica, 2009, 64: 882-905 19 Kruijff M, Van Der Heide E J, Ockels W J. Data analysis of a tethered spaceMail experiment. Journal of Spacecraft and Rockets, 2009, 46(6): 1272-1287 20 Hironori A F, Koga N. Experimental study on control of tethered subsatellite system in the rotational field. In: AIAA Guidance, Navigation, and Control Conference and Exhibit, Monterey, 1998 21 Kojima H, Furukawa Y, Trivailo P M. Experimental verification of periodic libration of tethered satellite system in elliptic orbit. Journal of Guidance, Control, and Dynamics, 2011, 34(2): 614-618 22 Takehara S, Terumichi Y, Nohmi M, et al. Numerical and experimental approaches on the motion of a tethered system. Journal of System Design and Dynamics, 2008,2(5): 1106-1117 23 Nohmi M, Tanikawa J, Hosoda T. Simulation analysis of a tethered space robot for space experiment on sounding rocket by JAXA/ISAS. In: Mechatronics and Automation (ICMA), 2010 International Conference, Xi'an, China, 2010 24 Nakaya K, Iai M, Omagari K, et al. Formation deployment control for spinning tethered formation flying simulations and ground experiment. In: AIAA Guidance, Navigation, and Control Conference and Exhibit. Providence, Rhode Island, 2004 25 Chung S, Kong E M, Miller D W. SPHERES Tethered formation flight testbed: Application to NASA's SPECS Mission. In: Proceedings of the SPIE, San Diego, CA,2005 26 Chung S, Kong E M, Miller D W. Dynamics and control of tethered formation flight spacecraft using the SPHERES testbed. In: 2005 AIAA Guidance, Navigation, and Control Conference and Exhibit, San Francisco, CA, 2005 27 文浩, 金栋平, 胡海岩. 绳系卫星收放控制地面实验研究. 振 动工程学报, 2010, 23(1): 7-11 28 Crouch D S, Vignoli M M. Shuttle tethered satellite system development program. In: Space Systems Technology Conference, Costa Mesa, CA, 1984 29 Chapter J J. Tethered satellite thermal design and test. In: 29th AIAA, Aerospace Sciences Meeting Reno, Nevada, 1991 30 Carroll J A. SEDS deployer design and flight performance. In: AIAA, Space Programs and Technologies Conference and Exhibit, Huntsville, AL, 1993 31 Bergamaschi S, Bonon F, Merlina P, et al. Theoretical and experimental investigation of TSS-1 dynamics. Acta Astronautica, 1994, 34: 69-82 32 Stone N H. Electrodynamic characteristics of the Tethered Satellite System during the TSS-1R mission. In: AIAA, Space Programs and Technologies Conference, Huntsville, AL, 1996 33 Gilchrist B E, Bilen S G, Choiniere E, et al. Ground simulations of electron current to wide probes for electrodynamic tethers. In: 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Salt Lake City, Utah,2001 34 Goldberg H R, Gilchrist B E. The Icarus student satellite project. Acta Astronautica, 2005, 56: 107-114 35 Menon C, Kruijff M, Vavouliotis A. Design and testing of a space mechanism for tether deployment. Journal of Spacecraft and Rockets, 2007, 44(4): 927-939 36 Hyslop A, Van Der Heide E J, Kruijff M, et al. A tethered upper stage for small launchers-preliminary analysis,design, and test. Progress in Propulsion Physics, 2009, 1:495-514 37 Higuchi K, Natori M C, Lwasa T, et al. A ground experiment of motion control of retrieving space tether: 38th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, and AIAA/ASME/AHS Adaptive Structures Forum. 1997,127(1): 715-719 38 Nohmi M, Tanikawa J, Hosoda T. Simulation analysis of a tethered space robot for space experiment on sounding rocket by JAXA ISAS. In: Proc. of International Conference on Mechatronics and Automation, Xi'an, China,2010 39 Nohmi M, Yoshida S. Experimental analysis for attitude control of a tethered space robot under microgravity. In: Proc. of 54th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law, Bremen, Germany, 2003 40 Nakamura Y, Hashimoto H. Ground test of tether deployment and retrieval along optimal path with a tether reeling mechanism designed for micro-class satellites. In: Proc. of 54th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law, Bremen, Germany, 2003 41 Yamanaka T, Iai M, Fujiwara K, et al. Design and microgravity experiment of separation mechanism for tether deployment. In: Proc. of 56th International Astronautical Congress, Fukuoka, Japan, 2005 42 Nakaya K, Iai M, Mori O, et al. On formation deployment for spinning tethered formation flying and experimental demonstration. Journal of the Japan Society for Aeronautical and Space Science, 2005, 53(616): 191-199 43 Matunaga S, Masumoto S, Yamanaka T. Retrieving dynamics and control of tethered sampling method for minorbody exploration. In: Proc. of AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Keystone, Colorado,2006 44 Lennert S, Cartmell M W P. Analysis and design of a friction brake for momentum exchange propulsion tethers. Acta Astronautica, 2005, 59(8): 1-8 45 Project Gemini 11-Press Kit. Washington D C: National Aeronautics and Space Administration, 1966 46 Team G M E. Gemini program mission report. Houston, Texas: National Aeronautics and Space Administration,1967 47 Craigboy. Gemini 11 Agena. 2011. http://en.wikipedia.org/wiki/File: Gemini 11 Agena.jpg 48 Manske M. Gemini 12 tethered stationkeeping. 2011. http://en. wikipedia.org/wiki/File:Gemini 12 tethered stationkeeping.jpg 49 Gilchrist B E, Banks P M, Neubert T, et al. Electron collection enhancement arising from neutral gas jets on a charged vehicle in the ionosphere.Journal of Geophysical Research, 1990, 95(3): 2469-2475 50 Tomlin D D, Mowery D K, Musetti B, et al. TSS mission 1 flight dynamic anomalies. In: Proceedings of the Fourth International Conference on Tethers in Space. Hampton, VA: Science and Technology Corp., 1995. 119-132 51 Cosmo M L, Lorenzini E C. Tethers in Space Handbook. Smithsonian Astrophysical Observatory, 1997 52 Bergamaschi S, Bonon F, Merlina P, et al. Theoretical and experimental investigation of TSS-1 dynamics. Acta Astronautica, 1994, 34: 69-82 53 Lorenzini E C, Bortolami S B, Rupp C C, et al. Control and flight performance of tethered satellite small expendable deployment system-I1. Journal of Guidance, Control, and Dynamics, 1996, 19(5): 1148-1156 54 Bricktop. STS-75 Tethered satellite system deployment.2006. http://en.wikipedia.org/wiki/File:STS-75 Tethered Satellite System deployment.jpg 55 Johnson L, Ballance J. Propulsive small expendable deployer system (ProSEDS) space demonstration, The Tether Technology Interchange Meeting, Huntsvihe, Al,1997 56 Wiedermann D G. Dynamic simulation of tethered satellite systems. Wien: eingereicht an der Technischen University “at Wien Fakult” at fur Maschinenbau, 2000 57 Gaff. NASAtether. 2007. http://en.wikipedia.org/wiki/File: NASAtether.gif 58 周以蕴. 绳系卫星系绳发电实验的成与败. 太空探索, 1996, (4): 22-23 59 Burke W J, Raitt W J, Thompson D C, et al. Shuttle charging by fixed energy beam emissions. Geophysical Research Letters, 1998, 25(5): 725-728 60 Victor M A, Brian E G, Scott D W, et al. Current collection model characterizing shuttle charging during the tethered satellite system missions. Journal of Spacecraft and Rockets, 2000, 37(2): 212-217 61 Winningham J D, Stone N H, Gurgiolo C A, et al. Suprathermal electrons observed on the TSS ‐ 1R satellite. Geophysical Research Letters, 1998, 25(4): 429-432 62 Williams S D, Gilchrist B E, Ag¨uero V M, et al. TSS ‐ 1R vertical electric fields: Long baseline measurements using an electrodynamic tether as a double probe. Geophysical Research Letters, 1998, 25(4): 445-448 63 Parker L W, Murphy B L. Potential buildup on an electron-emitting ionospheric satellite.Journal of Geophysical Research, 1967, 72(5): 1631-1636 64 Parker L W, Murphy B L. Potential buildup on an electron-emitting ionospheric satellite. Journal of Geophysical Research, 1967, 72(5): 1631-1636 65 Thompson D C, Bonifazi C, Gilchrist B E, et al. The current-voltage characteristics of a large probe in low Earth orbit: TSS-1R results. Geophysical Research Letters, 1998, 25(4): 413-416 66 Tether physics and survivability (TiPS) fact sheet. 1996. http://www.jya.com/nrotips.htm. 67 Purdy W, Coffey S, Barnds W J, et al. TiPS: Results of a tethered satellite experiment. In: Proceedings of the AAS/AIAA Astrodynamics Conference, Sun Valley, 1997 68 Alfriend K T, Barnds W J, Coffey S L, et al. Attitude and orbit determination of a tethered satellite system. In: AAS/AIAA Astrodynamics Specialist Conference, Halifax, Nova Scotia, 1995 69 Barnds W J, Coffey S, Davis M. Determination of TiPS libration using laser radar. In: Part of the SPIE Conference on Laser Radar Technology and Applications III. Orlando, Florida : 1998. 231-242 70 NOSS double and triple satellite formations. Naval Ocean Surveillance System. http://www.satobs.org/noss.html. 71 Knotnic. TiPS lg. 2006. http://en.wikipedia.org/wiki/File:TiPS lg.jpg 72 Levin E M. TiPS dynamics analysis. Acta Astronautica,2002, 50(9): 527-534 73 Gates S S, Koss S M, Zedd M F. Advanced tether experiment deployment failure. Journal of Spacecraft and Rockets, 2001, 38(1): 60-68 74 The YES programme. http://www.esa.int/esaMI/YES/SEMDTV8OY2F 0.html 75 Hoyt R, Slostad J. The multi-application survivability tether (MAST) experiment. In: Proceedings of the 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, 2003 76 The MAST experiment: A low-cost picosat experiment to demonstrate space tether technologies. http://www.tethers.com/Missions.html 77 The MAST experiment blog: A low-cost picosat experiment to demonstrate space tether technologies. http://www.tethers.com/MAST Blog.html 78 Mckee M. Inspector Gadget to Star in Space Tether Test.2007. http://www.newscientist.com/article/dn11466. 79 Young K. Experimental Space Tether Fails to Deploy.2007. http://www.newscientist.com/article/dn11836. 80 文浩, 陈辉, 金栋平, 等. 带可控臂绳系卫星释放及姿态控制. 力学学报, 2012, 44(2): 408-414
计量
- 文章访问数:2045
- HTML全文浏览量:118
- PDF下载量:2789
- 被引次数:0