参考文献
[1]余后满,张熇,黄晓峰,等,我国小天体探测任务设想(下)[J].国际太空,2021(9):4-9.
[2]Bierhaus,E B,et al.(2018).The OSIRIS-REx spacecraft and the touch-andgo sample acquisition mechanism(TAGSAM) [J].Space Science,Reviews,doi:10.1007/s11214-018-0521-6.
[3]Peypoudat V,Defoort B,Lacour D,et al.Development of a 3.2m long inflatable and rigidizable solar array breadboard[C].2005:AIAA 2005-1881.
[4]刘宇艳,孟秋影,谭惠丰,等.空间充气展开结构用刚化材料和刚化技术的研究现状[J].材料工程,2008(2):76-80.
[5]Cadogan D P,Scarborough S E.Rigidizable materials for use in gossamer space inflatable structures[C]//Proceedings of the 42nd AIAA/ASME/ASCEAHS/ASC Structures,Structural Dynamics,and Materials Conference&Exhibit,AIAA Gossamer Spacecraft Forum,Seattle,2001.
[6]Stohlman O R,Lappas V.Deorbitsail:a deployable sail for de-orbiting[C]//54th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference April 8-11,2013,Boston,Massachusetts,AIAA 2013-1806.
[7]Chen Y,You Z.Curved-profile deployable structures based on Bennett linkages[C]//48th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference 15th 23-26 April 2007,Honolulu,Hawaii,AIAA 2007-2115.
[8]Lin Tze Tan,Silas Norager.Deployable slotted shell reflector antennas[C]//48th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference 15th 23-26 April 2007,Honolulu,Hawaii,AIAA 2007-1846.
[9]Zheng Fei,Chen Mei,Zhao Lingyan,et al.Deploying ability analyses of a folded hoop-rib space deployable structure[C]//54th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference April 8-11,2013,Boston,Massachusetts,AIAA 2013-1830.
[10]Natori M C,Katsumata N,Okuizumi N.Deployable membrane structures with rolled-up booms and their deployment characteristics[C]//54th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference.April 8-11,2013,Boston,Massachusetts,AIAA-2013-1596.
[11]Juan M,Jeremy A,Emil V.Ardelean,creep effects and deployment characterization of rollable composite shell reflectors[C]//53rd AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference 20th AI 23-26 April 2012,Honolulu,Hawaii,AIAA 2012-1955.
[12]Hikari N,Yokosuka S.Rigidizable membranes for space inflatable structures[C]//43rd AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Con22-25 April 2002.
[13]毕朕.空间充气管展开过程仿真及模态分析[D].哈尔滨:哈尔滨工业大学,2006.
[14]Straubel M,Block J,Sinapius M.Deployable composite booms for various gossamer space structures[C]//52nd AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference 19th 4-7 April 2011,Denver,Colorado,AIAA 2011-2023.
[15]David P,Mark S,Grahne S.Deployment control mechanisms for inflatable space structures[C]//33rd Aerospace Mechanisms Conference,May 1999.
[16]王长国,杜星文,万志敏.薄膜褶皱的非线性屈曲有限元分析[J].计算力学学报,2007,24(3):269-274.
[17]周涛,谢志民,杜星文.空间充气支撑结构充气压力与刚度相关性研究[J].齐齐哈尔大学学报,2006,22(5):111-114.
[18]杨萍萍,冯长凯.可展开伸缩套管式伸展臂结构设计与分析[J].电子科技,2008,21(9):8-11.
[19]Leipold M,Runge H,Sickinger C.Large SAR membrane antennas with leightweight deployable booms[C]//Proceedings of the 28th ESA Antenna Workshop on Space Antenna Systems and Technol-ogies,ESA/ESTEC,2005.
[20]Straubel M,Block J,Sinapius M,et al.Deployable composite booms for various gossamer space structures[C]//52nd AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference,4-7 April 2011:AIAA 2011.
[21]Michael E Peterson,Thomas W Murphey.Large deformation bending of thin composite tape spring laminates[C]//54th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference.April 8-11,2013,Boston,Massachus-etts,AIAA 2013-1667.
[22]Witold M Sokolowski,Seng C Tan,Mark K Pryor.Lightweight shape memory self-deployable structures for gossamer applications[C]//45th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics&Materials Conference 19-22 April 2004,Palm Springs,California,AIAA 2004-1660.
[23]张展智,赵国伟,焦景勇,等.空间薄壁式伸展臂的展开仿真与卷曲方式研究[J].宇航学报,2013,34(3):299-307.
[24]Omer Soykasap.Deployment analysis of a self-deployable composite boom[C].Composite Structures,2009,89:374-381.
[25]Tang-Tat Ng and Thomas W.Murphey.A novel deployable boom with flexible hinges[C]//46th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics&Materials Conference,18-21 April 2005,Austin,Texas,AIAA 2005-2197.
[26]Sim A,Santer M.Analysis of a segmented compliant deployable boom for Cube-Sat magnetometer missions[C]//51st AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference 18th 12-15 April 2010,Orlando,Florida,AIAA 2010-2581.
[27]Karen H Lyle,Lucas G Horta.Deployment analysis of a simple tape-spring hinge using probabilistic methods[C]//53rd AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference20th AI 23-26 April 2012,Honolulu,Hawaii,AIAA 2012-1915.
[28]Bavdaz M,Gondoin P,Wallace K,et al.IXO system studies and technology preparation[C]//Submitted to SPIE,July 2009.
[29]Tibert G.Deployable tensegrity structures for space applications[C]//Royal Institute of Technology,Stockholm,2002.
[30]Gross D,Messner D.The able deployable articulated mast-enabling technology for the shuttle radar topography mission[C]//Proceedings of the 33rd Aerospace Mechanisms Symposium,1999.
[31]檀傈锰,白化同,程刚,等.大型可展收支撑臂模态试验研究[J].航天器工程,2012,21(6):125-130.
[32]马凯,程刚,彭慧莲,等.刚柔耦合状态下索杆式伸展臂多体动力学研究[J].航天器工程,2011,20(3):70-74.
[33]赵浩江,刘荣强,郭宏伟,等.桁架式支撑臂模态分析与振动主动控制研究[J].机械设计与制造,2012(4):4-6.
[34]赵孟良,吴开成,关富玲.空间可展桁架结构动力学分析[J].浙江大学学报(工学版),2005,39(11):1669-1674.
[35]刘荣强,郭宏伟,邓宗全.空间索杆铰接式伸展臂设计与试验研究[J].宇航学报,2009,30(1):315-320.
[36]郭宏伟,刘荣强,邓宗全,等.空间索杆式伸展臂展开过程力学分析与仿真[J].机械设计,2008,25(7):31-34.
[37]谢铁华,关富玲,苏斌,等.空间索杆式展开结构的动力学研究与分析[J].空间结构,2004,10(3):48-54.
[38]杨玉龙,张土乔,关富玲,等.连杆机构伸展臂结构方案的设计和研究[J].空间结构,1999,5(3):47-53.
[39]Matthew J Santer.Deployable CubeSat truss structures with compliant shape memory hinges[C]//54th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference April 8-11,2013,Boston,Massachusetts,AIAA 2013-1673.
[40]戈冬明,陈务军,付功义,等.铰接盘绕式空间伸展臂屈曲分析理论研究[J].工程力学,2008,25(6):176-180.
[41]薛纭,翁德玮.空间伸展臂由力螺旋控制的弹性盘绕折叠[J].机械设计与研究,2009,25(5):108-110.
[42]Hillebrandt M,Straubely M,Huhnez C et al.A new deployable truss for gossamer space structures[C]//53rd AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference 20th AI23-26 April 2012,Honolulu,Hawaii,AIAA 2012-1584.
[43]Puig L,Barton A,Rando N.A Review on large deployable structures for astrophy-sics missions[C]//Acta Astronautica 67,2010:12-26.
[44]陈务军,关富玲,陈向阳.可折叠航天结构展开动力学分析[J].计算力学学报,1999,16(4):397-402.
[45]Furuya H,Yokoyama J.Bending properties of bellows-type inflatable tube elements[C]//54th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference April 8-11,2013,Boston,Massachusetts,AIAA 2013-1865.
[46]Michael A Brown.Concept design of deployable isogrid booms[C]//52nd AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference 19th 4-7 April 2011,Denver,Colorado,AIAA 2011-2020.
[47]Natori M C,Nobuhisa Katsumata,Nobukatsu Okuizumi.Deployable membrane structures with rolled-up booms and their deployment characteristics[C]//54th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference.April 8-11,2013,Boston,Massachusetts,AIAA 2013-1596.
[48]Sickinger C,Herbeck L,Strohlein T,et al.Lightweight deployable booms:Design,manufacture,verification,and smart materials application[C]//55th International Astronautical Congress 2004,Vancouver,Canada.IAC-04-I.4.10.
[49]Irwin R J,Veen J,Buchner-Santos E,et al.Low-mass deployable spacecraft booms[C]//AIAA SPACE 2010 Conference&Exposition.2010-8926.
[50]Greschik G,Mikulas M M,Freeland R E.The nodal concept of deployment and the scale model testing of its application to a membrane antenna[C]//40th Structures,Structural Dynamics,and Materials Conference and Exhibit.1999:2546-2554.
[51]Campbell J,Smith S W,Main J A,et al.Staged microgravity deployment of a pressurizing scale-model spacecraft[J].Journal of Spacecraft and Rockets,2004,41(4):534-542.
[52]Clem A,Smith S,Main J.Experimental results regarding the inflation of unfolding cylindrical tubes[C]//Aiaa Applied Aerodynamics Conference,2001.
[53]刘晓峰,杜星文,谭惠丰.薄膜充气管充气展开特性试验[J].上海航天,2007,24(6):56-60.
[54]Welch A,Smith S,Main J.Experimental results regarding two-dimensional deployment of inflatable beams[J].Aiaa Journal,2013.
[55]Lou M,Fang H,Hsia L M.A combined analytical and experimental study on space inflatable booms[C]//IEEE Aerospace Conference Proceedings,2000 IEEE Aerospace Conference,Big Sky,MT,2000,2:503-512.
[56]Pappa R S,Lassiter J O,Ross B P.Structural dynamics experimental activities in ultralightweight and inflatable space structures[J].Journal of Spacecraft and Rockets,2003,40(1):15-23.
[57]管瑜.充气展开自硬化支撑管的设计与分析[D].杭州:浙江大学,2006.
[58]Tsunoda H,Senbokuya Y,Watanabe M.Deployment method of space inflatable structures using folding crease patterns[C]//Aiaa/asme/asce/ahs/asc Structures,Structural Dynamics,&Materials Conference,2006.
[59]Senda K,Ohta S,Igarashi Y,et al.Deploy experiment of inflatable tube using work hardening[C]//47th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th,2006.
[60]Fukuoka N.Deployment experiment on inflatable tubes of polygon folding under airplane microgravity[C]//International Astronautical Congress of the International Astronautical Federation,2013.
[61]D Lichodziejewski,Cravey R,Hopkins G.Inflatably deployed membrane waveguide array antenna for space[J].AIAA Journal,2003.
[62]Palisoc A L,Redell F H,Andersen G.Deployment and structural support of space membrane optics system using rigidizable conical booms[J].American Society of Civil Engineers,2004:946-953.
[63]Block J,Straubel M,Wiedemann M.Ultralight deployable booms for solar sails and other large gossamer structures in space[J].Acta Astronautica,2011.
[64]Colin Robert McInnes.Solar Sailing:Technology,dynamics and mission applications[M].Praxis Publishing Ltd,Chichester,UK,1999:36-40.
[65]Matloff G.The Solar Photon Sail:History,Current Status and Future Prospects[J].Space Chronicle:JBIS,2011,64(2):58-71.
[66]霍倩,饶哲,周春燕.太阳帆航天器展开结构技术综述[J].航天控制,2013,31(2):94-99.
[67]Leipold M,Eiden M,Garner C E,et al.Solar sail technology development and demonstration[J].Acta Astronautica,2003,52:317-326.
[68]Nishimura Y,Tsuda Y,Mori O,et al.The deployment experiment of solar sail With a sounding rocket[C]//55th International Astronautical Congress,Vancouver,Canada,2004:2278-2285.
[69]Takeuchi S,Tsuda Y,Mori O,et al.Deployment experiment result of solar sail using sounding rocket[C]//55th International Astronautical Congress,Vancouver,Canada,2004:468-475.
[70]陈罗婧.太阳帆航天器推进技术及其在轨试验[C]//第二十三届全国空间探测学术交流会,厦门,2010.
[71]黄河.宇宙1号太阳帆航天器[J].太阳能,2005(5):27-29.
[72]Alhorn D C,Casas J P,Agasid E F,et al.NanoSail-D:The small satellite that could[R].National Aeronautics and Space Administration,Huntsville,AL.George C.Marshall Space Flight Center,2011.
[73]Johnson L,Whorton M,Heaton A,et al.NanoSail-D:A solar sail demonstration mission[J].Acta astronautica,2011,68(5/6):571-575.
[74]Vaios Lappas,Nasir Adeli,Lourens Visagie,et al.CubeSail:A low cost Cube-Sat based solar sail demonstration mission[J].Advances in Space Research,2011,48:1890-1901.
[75]Muta A,Matunaga S,Okuizumi N.High vacuum experiment of spinning deloyment using scaled-down model for solar sail[C]//61st International Astronautical Congress,Prague,CZ,2010.
[76]Sawada H.Development of IKAROS mission system to expand Solar Power Sail[C]//61st International Astronautical Congress,Prague,CZ,2010.
[77]Tsuda Y,Mori O,Funase R,et al.Flight status of IKAROS Deep Space Solar Sail Demonstrator[C]//61st International Astronautical Congress,Prague,CZ,2010.
[78]Kawaguchi J,Mimasu Y,Mori O,et al.IKAROS-Ready for lift-off as the world's first solar sail demonstration in interplanetary space[C]//60th International Astronautical Congress,2009.
[79]沈自才,张帆,赵春晴,等.IKAROS太阳帆的关键技术分析与启示[J].航天器工程,2012,21(2):101-107.
[80]Mori O,Tsuda Y,Sawada H,et al.World's first mission of solar power sail by IKAROS[J].Space,Aeronautical and Navigational Electronics,2010,110(250):155-160.
[81]荣思远,刘家夫,崔乃刚,等.太阳帆航天器研究及其关键技术综述[J].上海航天,2011,28(2):53-62.
[82]王伟志.太阳帆技术综述[J].航天返回与遥感,2007,28(2):1-4.
[83]Kobayashi H,Kresling B,Vincent J F V.The geometry of unfolding tree leaves[J].The Royal Society,1998,265:147-154.
[84]Natori M,Shinjyuku,Kishimoto N,et al.Morphological concepts on efficient space structures with deployable and/or adaptive functions[C]//49th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference,Schaumburg,IL,2008.
[85]Furuya H,Inoue Y,Masuoka T.Deployment characteristics of rotationally skew fold membrane for spinning solar sail[C]//46th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics&Materials Conference,Austin,Texas,2005.
[86]Furuya H,Inoue Y.Dynamic properties of rotationally skew fold membrane for spinning solar sail[C]//47th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference,Newport,Rhode Island,2006.
[87]陈丽.薄膜抛物面反射器的圆柱式折叠研究[D].哈尔滨:哈尔滨工业大学,2007.
[88]冯维明,张敦福,王玲华.工程力学[M].北京:国防工业出版社,2008.
[89]Miura K,Natori M.2-D array experiment on board a space flyer unit[J].Space Solar Power Review,1985,5(4):345-356.
[90]Miura K.Method of packaging and deployment of large membranes in space[R].The Institute of Space and Astronautical,1980.
[91]Horner G C,Elliott M D.Fabrication and deployment approach for a Miura-Ori solar sail model[C]//43rd AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference,Denver,Colorado,2002.
[92]Wright T,Laue G,Horner G.A practical approach to large-area solar sail assembly utilizing the Miura-Ori folding technique[C]//39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,Huntsville,Alabama,2003.
[93]Papa A,Pellegrino S.Mechanics of systematically creased thin-film membrane structures[C]//46th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics&Materials Conference,Austin,Texas,2005.
[94]DeFocatiis DSA.,SD.G.Deployable membranes designed from folding tree leaves[J].Philosophical Transactions of the Royal Society.Mathematical,Physical,and Engineering Sciences,2002,360(1791):227-238.
[95]钱航,郑建华,李明涛,等.星际探测太阳帆行星和太阳借力轨道全局优化[J].国防科技大学学报,2016,38(1):137-142.
[96]钱航,郑建华,吴霞,等.非理想太阳帆受阴影影响的地球逃逸轨道探讨[J].航天器工程,2014,23(2):19-23.
[97]钱航,郑建华,于锡峥,等.太阳帆航天器悬浮轨道动力学与控制[J].空间科学学报,2013,33(4):458-464.
[98]钱航,郑建华,于锡峥,等.太阳帆航天器移位轨道设计[J].航天器工程,2012,21(6):25-29.
[99]钱航,郑建华.太阳帆航天器行星际轨道转移优化算法[J].空间控制技术与应用,2012,38(1):18-22.
[100]钱航,马鑫,郑建华,等.大型柔性太阳帆航天器姿态动力学建模研究[C]//全国第十六届空间及运动体控制技术学术会议,哈尔滨,2014:42-47.
[101]钱航,郑建华,于锡峥,等.考虑地影的非理想太阳帆地球逃逸轨道设计[C]//2013年航空宇航科学与技术全国博士生学术论坛,湖南长沙,2013:271-278.
[102]钱航,郑建华,于锡峥,等.飞向日心悬浮轨道的太阳帆航天器轨迹优化设计[C]//中国宇航学会深空探测技术委员会第十届学术年会,山西太原,2013:240-245.
[103]钱航,郑建华.太阳帆航天器悬浮轨道控制[C]//全国第十五届空间及运动体控制技术学术会议,吉林长春,2012:274-279.
[104]马鑫,杨萱,杨辰,等.太阳帆航天器姿态控制滚转轴稳定机设计[J].红外与激光工程,2014,43(S):72-77.
[105]Gong S P,Li J F.Fuel consumption for interplanetary missions of solar sailing[J].Science China Technological Sciences,2014,57(3):521-531.
[106]He J,Gong S P,Jiang F,et al.Time-optimal rendezvous transfer trajectory for restricted cone-angle range solar sails[J].Acta Mechanica Sinica,2014,30(5):628-635.
[107]Gong S,Li J.Solar sail halo orbit control using reflectivity control devices[J].Transactions of the Japan Society for Aeronautical and Space Sciences,2014,57(5):279-288.
[108]Gong S P,Li J F,Spin-stabilized solar sail for displaced solar orbits[J].Aerospace Science and Technology,2014,31(1):188-199.
[109]Hu X S,Gong S P,Li J F.Attitude stability criteria of axisymmetric Solar Sail[J].Advances in Space Research,2014,54(1):72-81.
[110]Zhang J,Wang T S,Gong S P.Influence of attitude control on orbital plane change for flexible solar sail[C]//The 3rd International Symposium on Solar Sail,Glasgow,2013.
[111]Mu J S,Gong S P,Li J F.Coupled attitude-orbit dynamics and control of reflectivity modulated solar sail GeoSail formation flying[C]//The 3rd International Symposium on Solar Sail,Glasgow,2013.
[112]He J,Gong S P,Li J F.The solar radiation pressure force models for a general sail surface shape[C]//The 3rd International Symposium on Solar Sail,Glasgow,2013.
[113]曾祥远,龚胜平,李俊峰,等.应用太阳帆悬停探测哑铃形小行星[C]//中国宇航学会深空探测技术专业委员会第十一届学术年会,2014.
[114]龚胜平,等,太阳帆航天器动力学与控制[M].北京:清华大学出版社,2014.
[115]高鸿,等.空间领域用高性能聚酰亚胺薄膜现状与发展[J].航天器环境工程,2014,31(3):248-253.
[116]Liu Y,Wu S,Wu Z,et al.Dynamic characteristics of geosynchronous Laplace orbit for space solar power station[J].Chinese Space Science&Technology,2016,36(5):1-8.
[117]Li S,Jiang X,Liu Y.Innovative Mars entry integrated navigation using modified multiple model adaptive estimation[J].Aerospace Science and Technology,2014,39:403-413.
[118]Liu Y,Yang C.Contrastive study on solar radiation pressure force model for solar sail[C]//33rd Chinese Control Conference(CCC).IEEE,2014.
[119]Liu Y,Zhou L,Cheng Z,et al.Simulation analysis of attitude-orbit-vibration coupling characteristics of the solar sail[C]//36rd Chinese Control Conference(CCC).IEEE,2017.
[120]Huang Xiaoqi,Wang Li,Liu Yufei,et al.Numerical analysis on the deployment and folding process of large-scale solar sail membrane[J].Zhongguo Kongjian Kexue Jishu(Chinese Space Science&Technology),2014,34(4):31-38.
[121]Liu Y,Cheng Z,Huang X.Solar sail interplanetary orbit design for multiple main belt asteroids exploration mission[C]//第37届 中 国 控 制 会 议,2018.
[122]Liu F,Hu Q,Liu Y.Attitude dynamics of electric sail from multibody perspective[J].American Institute of Aeronautics and Astronautics,2008,41:1-14.
[123]Wu S,LiuYufei,Radice Gianmarco,et al.Autonomous pointing control of a large satellite antenna subject to parametric uncertainty[J].Sensors,2017,17(3):560.
[124]Wang E,Wu S,Liu Y,et al.Distributed vibration control of a large solar power satellite[J].Astrodynamics,2019,3(2):189-203.
[125]霍明英,齐乃明,刘宇飞,等.电动帆改进推力模型及深空探测性能分析[J].动力学与控制学报,2018,16(2):6.
[126]Huo M,Zhang G,Qi N,et al.Initial trajectory design of electric solar wind sail based on finite Fourier series shape-based method[J].IEEE Transactions on Aerospace and Electronic Systems,2019,55(6):3674-3683.
[127]Wei J,Ma R,Liu Y,et al.Modal analysis and identification of deployable membrane structures[J].Acta Astronautica,2018,152:811-822.
[128]Cheng Z,Liu Y,Huang X,et al.Fold-deploument concept and prototype design for air-inflatable solar sail[C]//66th International Astronautical Congress,2015.
[129]Cheng Zhengai,Huang Xiaoqi,Liu Yufei,et al.High cost-effectiveness debris removal platform with self-assembly modular solar sail units[J].
[130]成正爱,刘宇飞,卫剑征,等.太阳帆折叠展开及支撑包装结构设计[C]//2014年可展开空间结构学术会议摘要集,2014.
[131]成正爱,柳青,冯展祖,等.空间带电粒子辐照与预应力耦合作用对功能形面薄膜结构性能影响研究[J].空间电子技术,2021,18(5):7.
[132]黄小琦,王立,刘宇飞,等.大型太阳帆薄膜折叠及展开过程数值分析[J].中国空间科学技术,2014,34(4):31-38.
[133]黄小琦,王立,刘宇飞,等.太阳帆表面薄膜空间电子辐照性能研究[J].真空与低温,2014,20(3):154-157.
[134]Huang Xiaoqi,Liu Yufei,Zhang Xinghua,et al.Ground testing of solar sail[C]//4th International Solar Sail symposium,2017.
[135]Huang Xiaoqi,Cheng Zhengai,Liu Yufei,et al.Study on solar sail folding patterns[C]//5th International Solar Sail symposium,2019.
[136]成正爱,刘宇飞,张兴华,等.面向采用充气辅助自回弹式支撑臂太阳帆的支撑包装结构:中国,CN103466197A[P].2013-12-25.
[137]刘海涛,刘宇飞,王立,等.一种具有电磁波收发能力的太阳光压推力获取结构:中国,CN104092005B[P].2016-06-29.
[138]杨辰,刘宇飞,张兴华,等.一种太阳帆结构有限元快速建模与后处理方法:中国,CN103886126A[P].2014-06-25.
[139]黄小琦,刘宇飞,王立,等.一种适于分块方形支撑杆型太阳帆帆面折叠技术:中国,CN103863580A[P].2014-06-18.
[140]刘宇飞,卫剑征,王立,等.一种用于大型薄膜结构展开的支撑臂:中国,CN104085541A[P].2014-10-08.
[141]刘宇飞,成正爱,黄小琦,等.一种利用太阳光压力驱动的深空太阳帆航天器:中国,CN104058105A[P].2014-09-24.
[142]杨辰,刘宇飞,张兴华,等.确定有效推进加速度折损的太阳帆瞬态动力学分析方法:中国,CN104484498A[P].2015-04-01.
[143]成正爱,黄小琦,刘宇飞,等.一种模块化太阳帆可组装重构的天基碎片清除平台和方法:中国,CN109279050A[P].2019-01-29.