在轨组装技术研究现状与发展趋势
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摘要
介绍了国内外在轨组装技术的研究现状,指出以模块化可重构航天器、大尺寸天线和光学载荷为典型目标的在轨组装技术已得到了广泛研究,提出模块及接口的通用化、提高组装效率和降低组装成本是在轨组装技术工程化应用的重点。归纳了在轨组装的关键技术,包括结构模块化及单元设计、在轨组装平台设计、在轨组装机器人以及在轨组装综合管理等。针对我国的技术现状,提出了我国开展在轨组装技术研究所需解决的问题和未来发展建议:应重点突破模块单元及连接组件的通用化、组装操作的高精度与高效率等瓶颈问题。
The development of on-orbit assembly technology in China and abroad were introduced in this paper and it was found that the on-orbit assembly technology targeting the modular reconfigurable spacecraft,large antennas and large observatories were widely studied. It was pointed out that the generalization of modules and interfaces,the improvement of assembly efficiency and the reduction of assembly cost were the key points of the engineering application. The key techniques of the on-orbit assembly including the design of modular structure and unit,the design of on-orbit assembly platform,the on-orbit assembly robot and the integrated on-orbit assembly management were summarized. Finally,problems to be solved in the future for the on-orbit assembly technology were analyzed and the research proposals were made based on the technical status of China such as focus on the generalization of modular unit and the connection components,focus on the high precision and efficiency of the assembly operation etc.
The development of on-orbit assembly technology in China and abroad were introduced in this paper and it was found that the on-orbit assembly technology targeting the modular reconfigurable spacecraft,large antennas and large observatories were widely studied. It was pointed out that the generalization of modules and interfaces,the improvement of assembly efficiency and the reduction of assembly cost were the key points of the engineering application. The key techniques of the on-orbit assembly including the design of modular structure and unit,the design of on-orbit assembly platform,the on-orbit assembly robot and the integrated on-orbit assembly management were summarized. Finally,problems to be solved in the future for the on-orbit assembly technology were analyzed and the research proposals were made based on the technical status of China such as focus on the generalization of modular unit and the connection components,focus on the high precision and efficiency of the assembly operation etc.
引文
[1]National aeronautics and space administration.Game changing development SALSSA:space assembly of large structureal system architectures[EB/OL].FS-2015-06-235-LaRC,2015.https://gameon.nasa.gov/files/2015/06/FS_SALSSA_150624.pdf.
[2]Mohan S,Miller D W.Operational impact of mass property update for on-orbit assembly[C]//Space Ops 2006 conference,AIAA 2006-5658:1-10.
[3]Lillie C.On-orbit assembly and servicing for future space observatories[C]//Space 2006,AIAA 2006-7251:1-12
[4]郭继峰,王平,崔乃刚.空间在轨装配任务规划[M].北京:国防工业出版社,2014:1-2.Guo Jifeng,Wang Ping,Cui Na-gang.Misson Planning for On-orbit Assembly[M].Beijing,2014:1-2.(in Chinese)
[5]蔡远文,郭会,李岩.航天器在轨组装技术进展[J].兵工自动化,2009,28(10):6-8.Cai Yuanwen,Guo Hui,Li Yan.Development of spacecraft on-orbit assembly technologies[J].Ordnance Industry Automation,2009,28(10):6-8.(in Chinese)
[6]芦瑶.空间在轨装配技术发展历程研究[D].哈尔滨:哈尔滨工业大学,2011.Lu Yao.The study of space on-orbit assembly technology[D].Harbin:Harbin institute of technology,2011.(in Chinese)
[7]Nishida S,Yoshikawa T.A New End-effector for On-orbit Assembly of a Large Reflector[C]//International Conference on Control,Automation,Robotics and Vision.IEEE,2006:1-6.
[8]Whittaker W,Urmson C,Staritz P,et al.Robotics for assembly,inspection,and maintenance of space macrofacolities[C]//AISS-2000-5288:1-6
[9]Hoyt R P,Cushing J I,Slostad J T,et al.Spider Fab:an architecture for self-fabricating space systems[C]//AIAA Space2013 Conference and Exposition,2013:1-17.
[10]侯欣宾.不同空间太阳能电站概念方案的比较研究[J].太阳能学报,2012(3):63-68.Hou Xin-bin.Analysis and comparison of various SPS concepts[J].ACTA Energiae Solaris Sinica,2012(3):63-68.(in Chinese)
[11]闫勇,金光.空间太阳能电站发展及研究[J].中国光学,2013,6(2):129-134.Yan Yong,Jin Guang.Development and research of solar power systems[J].Chinese Optics,2013,6(2):129-134.(in Chinese)
[12]崔瑛楠.美国空间在轨装配技术发展史[D].哈尔滨:哈尔滨师范大学,2012.Cui Yingnan.Development History of On-orbit Assembly Technology in United States of America[D].Harbin:Harbin Normal University,2012.(in Chinese)
[13]Randall C R,Porter B S,Stokley C,et al.Nextsat on-orbit experiences[C]//Sensors and systems for space applicationsⅡ,Proc.of SPIE Vol.6958.695807,2008.
[14]Adomeit A,Reimerdes H,Lakshmanan M,et al.Structural Concept and Design for Modular and Serviceable Spacecraft Systems[C]//AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference,2013.
[15]杨南基,黄献龙,王玉峰,等.细胞卫星体系的关键技术及启示[J].航天器环境工程,2015,32(4):434-439.Yang Nanji,Huang Xianlong,Wang Yufeng,et al.Key technologies of cellularized satellites building block system and its enlightenment[J].Spacecraft Environment Engineering,2015,32(4):434-439.(in Chinese)
[16]Van Wagenen J.Nova Wurks prepares self assembling spacecraft for LEO demonstration[OL].http://www.satellitetoday.com/technology/2016/01/27/novawurks-prepares-selfassembling-spacecraft-for-leo-demonstration/.
[17]Suzuki Y,Tsuchiya S,Okuyama T,et al.Mechanism for assembling antenna in space[J].IEEE Transactions on Aerospace and Electronic system,2001,37(1):254-265.
[18]Zheng F,Chen M,Li W,et al.Conceptual design of a new huge deployable antenna structure for space application[C]//2008 IEEE Aerospace Conference.Big Sky,MT,United states,2008.
[19]Meguro A,Shintate K,Usui M,et al.In-orbit deployment characteristics of large deployable antenna reflector onboard Engineering Test Satellite VIII[J].Acta Astronautica,2009,65(9):1306-1316.
[20]Freeland R E,Helms R G.Deployable antenna structures technologies[R/OL].Large space apertures workshop California institute of technology,Pasadena,California,2008.http://www.kiss.caltech.edu/workshops/apertures2008/talks/freeland.pdf.
[21]Ribble J W.Modular antenna design study[R].NASA Contractor Report 3316,1981:75-95.
[22]Vaughan D H.Modular reflector concept study[R].NASA Contractor Report 3411,1981:106.
[23]Cheryl L.Allen.Automated assembly of large space structures using an expert system executive[C]//NASA Langley Research Center;MS 152D,Hampton Va 23665-5225.
[24]Nishida S,Yoshikawa T.A new end-effector for on-orbit assembly of a large reflector[C]//International Conference on Control,Automation,Robotics and Vision,Icarcv 2006,Singapore,5-8 December 2006,Proceedings.DBLP,2006:1-6.
[25]NASA.Emerging space capabilities and tipping point summaries[EB/OL].(2015.12.19).https://www.nasa.gov/feature/emerging-space-capabilities-and-tipping-point-summaries/.
[26]Dorsey J,Doggett W,Hafley R,et al.An efficient and versatile means for assembling and manufacturing systems in space[C]//AIAA SPACE 2012 Conference&Exposition.2012.
[27]Oegerle W R,Purves L R,Budinoff J G,et al.Concept for a large scalable space telescope:in-space assembly[C]//SPIE Astronomical Telescopes+Instrumentation.International Society for Optics and Photonics,2006.
[28]Ebbets D,Green J.Architecture concept for a 10 m UV-optical space telescope[C]//SPIE Astronomical Telescopes+Instrumentation.International Society for Optics and Photonics,2006.
[29]Lake M S.Launching a 25-meter space telescope are astronauts a key to the next technically logical step after NGST?[C]//Presented at the 2001 IEEE Aerospace Conference,IEEE Paper No.460.
[30]Mahoney,M.J.Ibbott,A.C.A Large Deployable Reflector Assembly Scenario[R].NASA JPL D-5942,1988.
[31]Nishida S,Yoshikawa T.A new end-effector for on-orbit assembly of a large reflector[C]//International Conference on Control,Automation,Robotics and Vision,Icarcv 2006,Singapore,5-8 December 2006,Proceedings.DBLP,2006:1-6.
[32]方勇,郭桦,杜彦昌.DARPA 2015财年新增重点研究项目[J].装备参考,2014(20):1-5.Fang Yong,Guo Hua,Du Yanchang.The new focus of research projects of DARPA in 2015 fiscal year[J].Equipment reference,2014(20):1-5.(in Chinese)
[33]李云,刘海印,王聪.美国国防高级研究项目局2016财年航天预算项目[J].中国航天,2015(10):29-33.Liu Yun,Liu Haiyin,Wang cong.United States defense advanced research projects agency budget for fiscal 2016[J].Aerospace China,2015(10):29-33.(in Chinese)
[34]Watson J J,Collins T J,Bush H G.A history of astronaut construction of large space structures at NASA Langley Research Center[C]//Aerospace Conference Proceedings.IEEE Xplore,2002:7-3569-7-3587 vol.7.
[35]郭继峰,王平,崔乃刚.大型空间结构在轨装配技术的发展[J].导弹与航天运载技术,2006(3):28-35.Guo Jifeng,Wang Ping,Cui Naigang.Development of on-orbit assembly of large space structures[J].Missile and Space Vehicle,2006(3):28-35.(in Chinese)
[36]Whittaker W L,Urmson C,Staritz P.Robotics for assembly,inspection and maintenance of space macrofacilities[R].AIAA-2000-5288,2000.
[37]Bridgwater L,Ambrose R,Diftler M,et al.Symbiotic robots for space based construction and maintenance[R].AIAA2006-7394,2006.
[38]Yim M,Shen W M,Salemi B,et al.Modular self-reconfigurable robot systems:challenges and opportunities for the future[J].IEEE Robotics&Automation Magazine,2012,14(1):43-52.
[39]Hoyt R P,Cushing J I,Slostad J T,et al.Spider Fab:an architecture for self-fabircating space systems[C]//AIAA Space2013 Conference and Exposition,2013:1-17.
[40]Pu Jialun.Model design of On-orbit antonomous assembly multi-robot systems[C]//2010 2dn International Conference on Industrial and Information Systems,978-1-4244-8217-7,2010 IEEE:472-475.
[41]Werner D.NASA,made in space think big with archinaut,a robotic 3D printing demo bound for ISS[J/OL].(2016.2.23).http://spacenews.com/nasa-made-in-spacethink-big-with-archinaut-a-robotic-3d-printing-demo-boundfor-iss/.
[42]张庆利,倪风雷,朱映远,等.三手指空间机器人末端执行器的柔顺抓握策略[J].机器人,2011,22(4):427-433.Zhu Qingli,Ni Fenglei,Zhu Yingyuan,et al.Compliant grasp strategy for three-fingered space robot end-effector[J].Robot,2011,22(4):427-433.(in Chinese)
[43]张庭,姜力,刘宏.仿生假手抓握力控制策略[J].机器人,2012,34(2):190-196.Zhang Ting,Jiang Li,Liu Hong.A grasping force control strategy for anthropomorphic prosthetic hand[J].Robot,2012,34(2):190-196.(in Chinese)
[44]Huo Xijian,Liu Yiwei,Jiang Li,et al.Inverse kinematic optimizations of 7R humanoid arms based on a joint parameterization[C]//International Conference on Mechatronics and Automation,978-1-4799-3977-0/14 2014 IEEE.
[45]郭继峰,王平,崔乃刚.大型空间桁架结构装配序列的分层规划方法[J].哈尔滨工业大学学报,2008,40(3):350-353.Guo Ji-feng,Wang Ping,Cui Nai-gang.Hierarchical planning method for assembly sequences of large space truss structures[J].Journal of Harbin Institute of Technology,2008,40(3):350-353.(in Chinese)
[46]郭继峰,王平,程兴,崔乃刚.一种用于空间在轨装配的两级递阶智能规划算法[J].宇航学报,2008,29(3):1059-1063.Guo Jifeng,Wang Ping,Cheng Xing,Cui Naigang.Tow-level hierarchical intelligent planning algorithm for on-orbit assembly[J].Journal of Astronautics,2008,29(3):1059-1063.(in Chinese)
[47]刘兆晶.模块化可展开抛物面天线支撑机构设计与研制[D].哈尔滨:哈尔滨工业大学,2011.Liu Zhaojing.Design and Manufacture of Supporting Structure for Modular Deployable Parabpolic Antenna[D].Harbin:Harbin Institute of Technology,2011.(in Chinese)
[48]田大可.模块化空间可展开天线支撑桁架设计与实验研究[D].哈尔滨:哈尔滨工业大学,2011.Tian Dake.Design and Experiment in research on Truss Structure for Modular Space Deployable Antenna[D].Harbin:Harbin Institute of Technology.(in Chinese)
[49]胡其彪.空间可伸展结构的设计与动力学分析研究[D].杭州:浙江大学,2001.Hu Qi Biao.Structure Design and Kinematic&Dynamic Analysis Research for Spatial Deployable Structures[D].Hangzhou:Zhejiang University,2001.(in Chinese)
[50]李团结,马小飞,华岳,等.大型空间天线在轨装配技术[J].载人航天,2013,19(1):86-90.Li Tuanjie,Ma Xiaofei,Hua Yue,et al.On-orbit assembly technology of large space antennas[J].Manned Spaceflight,2013,19(1):86-90.(in Chinese)
[51]黄攀峰,常海涛,鹿振宇,等.面向在轨服务的可重构细胞卫星关键技术与展望[J].宇航学报,2016,37(1):1-10.Huang Panfeng,Chang Haitao,Lu Zhenyu,et al.Key techniques od on-orbit service-oriented reconfigurable cellularized satellite and its prospects[J].Journal of Astronautics,2016,37(1):1-10.(in Chinese)
[52]马尚君,刘更,吴立言,等.航天器结构的模块化设计方法综述[J].机械科学与技术,2011,30(6):960-967.Ma Shangjun,Liu geng,Wu Liyan,et al.A revire of the modular design methods for spacecraft structure[J].Mechanical Science and Technology for Aerosoace Engineering,2011,30(6):960-967.(in Chinese)
[53]罗浩,刘更,马尚君,等.可在轨展开的航天器模块化结构设计分析平台研究[J].机械科学与技术,2012,31(1):29-33.Luo Hao,Liu Geng,Ma Shangjun,et al.Study on the modular design and analysis platform for spacecraft deployable onorbit[J].Mechanical Science and Technology for Aerosoace Engineering,2012,31(1):29-33.(in Chinese)
[54]付伟达,张士峰,张锐,等.小卫星测控的模块化自动测试系统构建[J].航天器工程,2013,22(2):104-107.Fu Weida,Zhang Shifeng,Zhang Rui,et al.Construction of modular automatic test systems for small satellite TT&C[J].Spacesraft Engineering,2013,22(2):104-107.(in Chinese)
[55]高朝辉,王俊峰,童科伟,等.重型运载火箭发射空间太阳能电站相关技术问题分析[J].导弹与航天运载技术,2016(2):51-54.Gao Chaohui,Wang Junfeng,Tong Kewei,et al.Technology analysis of the questions on space solar-power station launching by the heavy launch vehicles[J].Missiles and Space Vehicles,2016(2):51-54.(in Chinese)
[56]Kenner W S,Rhodes M D,Fichter W B.Component count and preliminary assembly considerations for large space truss structures[R].NASA Technical Memorandum 102604,1990.
[57]Rule W K,Thomas F P.Design of a welded joint for robotic,on-orbit assembly of space trusses[R].NASA TM-108380,1992.
[2]Mohan S,Miller D W.Operational impact of mass property update for on-orbit assembly[C]//Space Ops 2006 conference,AIAA 2006-5658:1-10.
[3]Lillie C.On-orbit assembly and servicing for future space observatories[C]//Space 2006,AIAA 2006-7251:1-12
[4]郭继峰,王平,崔乃刚.空间在轨装配任务规划[M].北京:国防工业出版社,2014:1-2.Guo Jifeng,Wang Ping,Cui Na-gang.Misson Planning for On-orbit Assembly[M].Beijing,2014:1-2.(in Chinese)
[5]蔡远文,郭会,李岩.航天器在轨组装技术进展[J].兵工自动化,2009,28(10):6-8.Cai Yuanwen,Guo Hui,Li Yan.Development of spacecraft on-orbit assembly technologies[J].Ordnance Industry Automation,2009,28(10):6-8.(in Chinese)
[6]芦瑶.空间在轨装配技术发展历程研究[D].哈尔滨:哈尔滨工业大学,2011.Lu Yao.The study of space on-orbit assembly technology[D].Harbin:Harbin institute of technology,2011.(in Chinese)
[7]Nishida S,Yoshikawa T.A New End-effector for On-orbit Assembly of a Large Reflector[C]//International Conference on Control,Automation,Robotics and Vision.IEEE,2006:1-6.
[8]Whittaker W,Urmson C,Staritz P,et al.Robotics for assembly,inspection,and maintenance of space macrofacolities[C]//AISS-2000-5288:1-6
[9]Hoyt R P,Cushing J I,Slostad J T,et al.Spider Fab:an architecture for self-fabricating space systems[C]//AIAA Space2013 Conference and Exposition,2013:1-17.
[10]侯欣宾.不同空间太阳能电站概念方案的比较研究[J].太阳能学报,2012(3):63-68.Hou Xin-bin.Analysis and comparison of various SPS concepts[J].ACTA Energiae Solaris Sinica,2012(3):63-68.(in Chinese)
[11]闫勇,金光.空间太阳能电站发展及研究[J].中国光学,2013,6(2):129-134.Yan Yong,Jin Guang.Development and research of solar power systems[J].Chinese Optics,2013,6(2):129-134.(in Chinese)
[12]崔瑛楠.美国空间在轨装配技术发展史[D].哈尔滨:哈尔滨师范大学,2012.Cui Yingnan.Development History of On-orbit Assembly Technology in United States of America[D].Harbin:Harbin Normal University,2012.(in Chinese)
[13]Randall C R,Porter B S,Stokley C,et al.Nextsat on-orbit experiences[C]//Sensors and systems for space applicationsⅡ,Proc.of SPIE Vol.6958.695807,2008.
[14]Adomeit A,Reimerdes H,Lakshmanan M,et al.Structural Concept and Design for Modular and Serviceable Spacecraft Systems[C]//AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference,2013.
[15]杨南基,黄献龙,王玉峰,等.细胞卫星体系的关键技术及启示[J].航天器环境工程,2015,32(4):434-439.Yang Nanji,Huang Xianlong,Wang Yufeng,et al.Key technologies of cellularized satellites building block system and its enlightenment[J].Spacecraft Environment Engineering,2015,32(4):434-439.(in Chinese)
[16]Van Wagenen J.Nova Wurks prepares self assembling spacecraft for LEO demonstration[OL].http://www.satellitetoday.com/technology/2016/01/27/novawurks-prepares-selfassembling-spacecraft-for-leo-demonstration/.
[17]Suzuki Y,Tsuchiya S,Okuyama T,et al.Mechanism for assembling antenna in space[J].IEEE Transactions on Aerospace and Electronic system,2001,37(1):254-265.
[18]Zheng F,Chen M,Li W,et al.Conceptual design of a new huge deployable antenna structure for space application[C]//2008 IEEE Aerospace Conference.Big Sky,MT,United states,2008.
[19]Meguro A,Shintate K,Usui M,et al.In-orbit deployment characteristics of large deployable antenna reflector onboard Engineering Test Satellite VIII[J].Acta Astronautica,2009,65(9):1306-1316.
[20]Freeland R E,Helms R G.Deployable antenna structures technologies[R/OL].Large space apertures workshop California institute of technology,Pasadena,California,2008.http://www.kiss.caltech.edu/workshops/apertures2008/talks/freeland.pdf.
[21]Ribble J W.Modular antenna design study[R].NASA Contractor Report 3316,1981:75-95.
[22]Vaughan D H.Modular reflector concept study[R].NASA Contractor Report 3411,1981:106.
[23]Cheryl L.Allen.Automated assembly of large space structures using an expert system executive[C]//NASA Langley Research Center;MS 152D,Hampton Va 23665-5225.
[24]Nishida S,Yoshikawa T.A new end-effector for on-orbit assembly of a large reflector[C]//International Conference on Control,Automation,Robotics and Vision,Icarcv 2006,Singapore,5-8 December 2006,Proceedings.DBLP,2006:1-6.
[25]NASA.Emerging space capabilities and tipping point summaries[EB/OL].(2015.12.19).https://www.nasa.gov/feature/emerging-space-capabilities-and-tipping-point-summaries/.
[26]Dorsey J,Doggett W,Hafley R,et al.An efficient and versatile means for assembling and manufacturing systems in space[C]//AIAA SPACE 2012 Conference&Exposition.2012.
[27]Oegerle W R,Purves L R,Budinoff J G,et al.Concept for a large scalable space telescope:in-space assembly[C]//SPIE Astronomical Telescopes+Instrumentation.International Society for Optics and Photonics,2006.
[28]Ebbets D,Green J.Architecture concept for a 10 m UV-optical space telescope[C]//SPIE Astronomical Telescopes+Instrumentation.International Society for Optics and Photonics,2006.
[29]Lake M S.Launching a 25-meter space telescope are astronauts a key to the next technically logical step after NGST?[C]//Presented at the 2001 IEEE Aerospace Conference,IEEE Paper No.460.
[30]Mahoney,M.J.Ibbott,A.C.A Large Deployable Reflector Assembly Scenario[R].NASA JPL D-5942,1988.
[31]Nishida S,Yoshikawa T.A new end-effector for on-orbit assembly of a large reflector[C]//International Conference on Control,Automation,Robotics and Vision,Icarcv 2006,Singapore,5-8 December 2006,Proceedings.DBLP,2006:1-6.
[32]方勇,郭桦,杜彦昌.DARPA 2015财年新增重点研究项目[J].装备参考,2014(20):1-5.Fang Yong,Guo Hua,Du Yanchang.The new focus of research projects of DARPA in 2015 fiscal year[J].Equipment reference,2014(20):1-5.(in Chinese)
[33]李云,刘海印,王聪.美国国防高级研究项目局2016财年航天预算项目[J].中国航天,2015(10):29-33.Liu Yun,Liu Haiyin,Wang cong.United States defense advanced research projects agency budget for fiscal 2016[J].Aerospace China,2015(10):29-33.(in Chinese)
[34]Watson J J,Collins T J,Bush H G.A history of astronaut construction of large space structures at NASA Langley Research Center[C]//Aerospace Conference Proceedings.IEEE Xplore,2002:7-3569-7-3587 vol.7.
[35]郭继峰,王平,崔乃刚.大型空间结构在轨装配技术的发展[J].导弹与航天运载技术,2006(3):28-35.Guo Jifeng,Wang Ping,Cui Naigang.Development of on-orbit assembly of large space structures[J].Missile and Space Vehicle,2006(3):28-35.(in Chinese)
[36]Whittaker W L,Urmson C,Staritz P.Robotics for assembly,inspection and maintenance of space macrofacilities[R].AIAA-2000-5288,2000.
[37]Bridgwater L,Ambrose R,Diftler M,et al.Symbiotic robots for space based construction and maintenance[R].AIAA2006-7394,2006.
[38]Yim M,Shen W M,Salemi B,et al.Modular self-reconfigurable robot systems:challenges and opportunities for the future[J].IEEE Robotics&Automation Magazine,2012,14(1):43-52.
[39]Hoyt R P,Cushing J I,Slostad J T,et al.Spider Fab:an architecture for self-fabircating space systems[C]//AIAA Space2013 Conference and Exposition,2013:1-17.
[40]Pu Jialun.Model design of On-orbit antonomous assembly multi-robot systems[C]//2010 2dn International Conference on Industrial and Information Systems,978-1-4244-8217-7,2010 IEEE:472-475.
[41]Werner D.NASA,made in space think big with archinaut,a robotic 3D printing demo bound for ISS[J/OL].(2016.2.23).http://spacenews.com/nasa-made-in-spacethink-big-with-archinaut-a-robotic-3d-printing-demo-boundfor-iss/.
[42]张庆利,倪风雷,朱映远,等.三手指空间机器人末端执行器的柔顺抓握策略[J].机器人,2011,22(4):427-433.Zhu Qingli,Ni Fenglei,Zhu Yingyuan,et al.Compliant grasp strategy for three-fingered space robot end-effector[J].Robot,2011,22(4):427-433.(in Chinese)
[43]张庭,姜力,刘宏.仿生假手抓握力控制策略[J].机器人,2012,34(2):190-196.Zhang Ting,Jiang Li,Liu Hong.A grasping force control strategy for anthropomorphic prosthetic hand[J].Robot,2012,34(2):190-196.(in Chinese)
[44]Huo Xijian,Liu Yiwei,Jiang Li,et al.Inverse kinematic optimizations of 7R humanoid arms based on a joint parameterization[C]//International Conference on Mechatronics and Automation,978-1-4799-3977-0/14 2014 IEEE.
[45]郭继峰,王平,崔乃刚.大型空间桁架结构装配序列的分层规划方法[J].哈尔滨工业大学学报,2008,40(3):350-353.Guo Ji-feng,Wang Ping,Cui Nai-gang.Hierarchical planning method for assembly sequences of large space truss structures[J].Journal of Harbin Institute of Technology,2008,40(3):350-353.(in Chinese)
[46]郭继峰,王平,程兴,崔乃刚.一种用于空间在轨装配的两级递阶智能规划算法[J].宇航学报,2008,29(3):1059-1063.Guo Jifeng,Wang Ping,Cheng Xing,Cui Naigang.Tow-level hierarchical intelligent planning algorithm for on-orbit assembly[J].Journal of Astronautics,2008,29(3):1059-1063.(in Chinese)
[47]刘兆晶.模块化可展开抛物面天线支撑机构设计与研制[D].哈尔滨:哈尔滨工业大学,2011.Liu Zhaojing.Design and Manufacture of Supporting Structure for Modular Deployable Parabpolic Antenna[D].Harbin:Harbin Institute of Technology,2011.(in Chinese)
[48]田大可.模块化空间可展开天线支撑桁架设计与实验研究[D].哈尔滨:哈尔滨工业大学,2011.Tian Dake.Design and Experiment in research on Truss Structure for Modular Space Deployable Antenna[D].Harbin:Harbin Institute of Technology.(in Chinese)
[49]胡其彪.空间可伸展结构的设计与动力学分析研究[D].杭州:浙江大学,2001.Hu Qi Biao.Structure Design and Kinematic&Dynamic Analysis Research for Spatial Deployable Structures[D].Hangzhou:Zhejiang University,2001.(in Chinese)
[50]李团结,马小飞,华岳,等.大型空间天线在轨装配技术[J].载人航天,2013,19(1):86-90.Li Tuanjie,Ma Xiaofei,Hua Yue,et al.On-orbit assembly technology of large space antennas[J].Manned Spaceflight,2013,19(1):86-90.(in Chinese)
[51]黄攀峰,常海涛,鹿振宇,等.面向在轨服务的可重构细胞卫星关键技术与展望[J].宇航学报,2016,37(1):1-10.Huang Panfeng,Chang Haitao,Lu Zhenyu,et al.Key techniques od on-orbit service-oriented reconfigurable cellularized satellite and its prospects[J].Journal of Astronautics,2016,37(1):1-10.(in Chinese)
[52]马尚君,刘更,吴立言,等.航天器结构的模块化设计方法综述[J].机械科学与技术,2011,30(6):960-967.Ma Shangjun,Liu geng,Wu Liyan,et al.A revire of the modular design methods for spacecraft structure[J].Mechanical Science and Technology for Aerosoace Engineering,2011,30(6):960-967.(in Chinese)
[53]罗浩,刘更,马尚君,等.可在轨展开的航天器模块化结构设计分析平台研究[J].机械科学与技术,2012,31(1):29-33.Luo Hao,Liu Geng,Ma Shangjun,et al.Study on the modular design and analysis platform for spacecraft deployable onorbit[J].Mechanical Science and Technology for Aerosoace Engineering,2012,31(1):29-33.(in Chinese)
[54]付伟达,张士峰,张锐,等.小卫星测控的模块化自动测试系统构建[J].航天器工程,2013,22(2):104-107.Fu Weida,Zhang Shifeng,Zhang Rui,et al.Construction of modular automatic test systems for small satellite TT&C[J].Spacesraft Engineering,2013,22(2):104-107.(in Chinese)
[55]高朝辉,王俊峰,童科伟,等.重型运载火箭发射空间太阳能电站相关技术问题分析[J].导弹与航天运载技术,2016(2):51-54.Gao Chaohui,Wang Junfeng,Tong Kewei,et al.Technology analysis of the questions on space solar-power station launching by the heavy launch vehicles[J].Missiles and Space Vehicles,2016(2):51-54.(in Chinese)
[56]Kenner W S,Rhodes M D,Fichter W B.Component count and preliminary assembly considerations for large space truss structures[R].NASA Technical Memorandum 102604,1990.
[57]Rule W K,Thomas F P.Design of a welded joint for robotic,on-orbit assembly of space trusses[R].NASA TM-108380,1992.