中文核心期刊

中国科技核心期刊

中国科学引文数据库（CSCD）来源期刊

中国高校百佳科技期刊

中国宇航学会深空探测技术专业委员会会刊

高级检索

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

太阳帆航天器的关键技术

胡海岩

downloadPDF
文章导航> 深空探测学报(中英文）> 2016> 3(4): 334-344
胡海岩. 太阳帆航天器的关键技术[J]. 深空探测学报(中英文）, 2016, 3(4): 334-344. doi: 10.15982/j.issn.2095-7777.2016.04.005
引用本文: 胡海岩. 太阳帆航天器的关键技术[J]. 深空探测学报(中英文）, 2016, 3(4): 334-344.doi:10.15982/j.issn.2095-7777.2016.04.005
shu
HU Haiyan. Key Technologies of Solar Sail Spacecraft[J]. Journal of Deep Space Exploration, 2016, 3(4): 334-344. doi: 10.15982/j.issn.2095-7777.2016.04.005
Citation: HU Haiyan. Key Technologies of Solar Sail Spacecraft[J].Journal of Deep Space Exploration, 2016, 3(4): 334-344.doi:10.15982/j.issn.2095-7777.2016.04.005
shu

太阳帆航天器的关键技术

doi:10.15982/j.issn.2095-7777.2016.04.005

  • bob手机在线登陆宇航学院 飞行器动力学与控制教育部重点实验室, 北京 100081

Key Technologies of Solar Sail Spacecraft

  • MOE Key Lab of Dynamics and Control of Flight Vehicles, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

  • 摘要:将太阳帆航天器所涉及的关键技术划分为4个方面：总体设计、轨道和姿态动力学与控制、太阳帆材料及其性能、太阳帆折叠与展开。针对每项关键技术，基于对国外长期研究结果进行分析并阐述主要技术特征，梳理国内相关研究进展，包括笔者与合作者的研究成果，分析存在的主要问题。根据上述分析，指出我国发展太阳帆航天器应该重视的若干问题。
    Abstract:This article surveys the key technologies of solar sail spacecraft in the following four aspects,the global design, the orbit and altitude controls,the solar sail materials and their properties,and the folding and deployment of solar sails. For each aspect,the article summarizes the major contents and features according to the previous studies abroad and presents the recent advances in China,including the recent studies of the author's laboratory. Based on the successful achievements and detailed analysis on open problems,the article addresses some important issues,which will receive more attention when China develops solar sail spacecraft.
  • [1] Tsuda Y,Mori O,Funase R,et al. Achievement of IKAROS-Japanese deep space solar sail demonstration mission[J]. Acta Astronautica,2013,88(1):183-188.
    [2] Johnson L,Whorton M,Heaton A. Nano sail-d:a solar sail demonstration mission[J]. Acta Astronautica,2011,68(5-6):571-575.
    [3] 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. Shen Z C,Zhang F,Zhao C Q,et al. Key technology analysis and enlightenment of IKAROS solar sail[J]. Spacecraft Engineering,2012,21(2):101-107.
    [4] Wie B. Hovering Control of a solar sail gravity tractor spacecraft for asteroid deflection[C]//Proceedings of the 2007 Planetary Defense Conference.[S.l.]:[s.n.],2007,AAS-07-145.
    [5] Gao Y T,Wu J Y. The optimal control for the tethered system formed by an asteroid and a solar sail,Advances in Space Research[J]. 2016,57:1002-1014.
    [6] 宋斌,颜根廷,张化岚,等. 太阳帆航天器系统初步设想[C]//中国宇航学会深空探测技术专业委员会第八届学术年会论文集. 上海:CDSET,2011,51-58.
    [7] 钱航,郑建华,李明涛. 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. Qian H,Zheng J H,Li M T. Global optimization of solar sail gravity assist and solar photonic assist trajectory for interstellar mission[J]. Journal of National University of Defense Technology,2016,38(1):137-142.
    [8] 马鑫,杨萱,郑建华,等. 太阳帆柔性结构动力学仿真分析[J]. 空间控制技术与应用,2014,40(3):36-46. Ma X,Yang X,Zheng J H,et al. Simulation and analysis for the flexible structure of solar sail spacecraft[J]. Aerospace Contrd and Application,2014,40(3):36-46.
    [9] 刘宇飞,荣思远,沈凡,等. 太阳帆探测器构型选择研究[C]//中国宇航学会深空探测技术专业委员会第十届学术年会论文集. 北京:CDSET,2013,51-58.
    [10] 钱航,郑建华,吴霞,等. 太阳帆推进任务的快速仿真方法[J]. 空间控制技术与应用,2016,42(2):8-13. Qian H,Zheng J H,Wu X,et al. Method of mission analysis for solar sail exploration based on STK[J]. Aerospace Contrd and Application,2016,42(2):8-13.
    [11] Wie B. Solar Sail attitude control and dynamics,Part 1[J]. Journal of Guidance,Control and Dynamics. 2004,27(4):526-535.
    [12] Wie B. Solar Sail attitude control and dynamics,Part 2[J]. Journal of Guidance,Control and Dynamics. 2004,27(4):536-544.
    [13] 韩艳铧,张震亚,贾杰. 太阳帆航天器姿态控制技术综述[J]. 航天器环境工程,2013,30(6):667-674. Han Y H,Zhang Z Y,Jia J. Review of attitude control techniques for solar spacecraft[J]. Space Environment Engineering,2013,30(6):667-674.
    [14] 龚胜平. 太阳帆航天器动力学与控制研究[D]. 北京:清华大学,2009.
    [15] 曾祥远. 深空探测太阳帆航天器新型轨道设计[D]. 北京:清华大学,2013.
    [16] Gong S P,Li J F. Orbital motions of a solar sail around the L2 Earth-Moon libration point[J]. Journal of Guidance,Control and Dynamics,2014,37(4),349-356.
    [17] Gong S P,Li J F. Equilibria near asteroids for solar sails with reflection control devices[J]. Astrophysics in Space Science,2015,355:213-223
    [18] Gong S P,Li J F. Optimal attitude maneuver of an axisymmetric spinning solar sail[J]. IEEE Transactions on Aerospace and Electronic Systems,2016,51(2):1462-1474.
    [19] 史晓宁. 太阳帆深空探测轨道控制与优化方法研究[D]. 哈尔滨:哈尔滨工业大学,2013.
    [20] 史晓宁,荣思远,白瑜亮. 太阳帆航天器行星分段捕获控制方法研究[J]. 2016,上海航天,33(2):87-93. Shi J N,Rong S Y,Bai Y L. Study on solar sail planet-centered segmented capture method[J]. 2016,Aerospace Shanghai,33(2):87-93.
    [21] 刘家夫. 复杂机构结构太阳帆航天器动力学建模与控制问题研究[D]. 哈尔滨:哈尔滨工业大学,2012.
    [22] 罗超,郑建华,高东. 太阳帆航天器的轨道动力学和轨道控制研究[J]. 宇航学报,2009,30(6):2111-2117. Luo C,Zheng J H,Gao D. Study on orbit dynamics and control of solar-sail spacecraft[J]. Journal of Astronautics,2009,30(6):2111-2117.
    [23] 罗超,郑建华. 太阳帆日心定点悬浮转移轨道设计[J]. 航天器工程,2014,23(3):12-17. Luo C,Zheng J H. Solar sail trajectory design for transferring heliocentric fixed displaced orbit[J]. Spacecraft Engineering,2014,23(3):12-17.
    [24] 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. Qian H,Zheng J H,Wu X,et al. Preliminary discussion on escape trajectories with shadow for nonideal solar sailing[J]. Spacecraft Engineering,2014,23(2):19-23.
    [25] Yokota R,Miyauchi M. Development of heat sealable polyimide thin films with high space environmental Stability for Solar Sail IKAROS Membrane[C]//Protection of Materials and Structures from the Space Environment. Berlin:Springer-Verlag,2014:303-316.
    [26] Ruth H P,Paiul A C. Advanced materials for space application[J]. Acta Astronautica,2007,61(11-12):1121-1129.
    [27] Bryant R G,Seaman S T,Wilkie W K. Selection and manufacturing of membrane materials for solar sails[C]//Advances in Solar Sailing. 2014. Berlin:Springer-Verlag,525-540.
    [28] Albarado T L. Electron Exposure measurements of candidate solar sail materials[J]. ASME Journal of Solar Energy Engineering,2005,127(1):125-130.
    [29] Shimamura H,Yamagata I. Degradation of mechanical properties of polyimide film exposed to space environment[J]. Journal of Spacecraft and Rockets,2009,46(1):15-21.
    [30] 黄小琦,王立,刘宇飞. 太阳帆飞行器帆体结构材料选用分析[C]//中国宇航学会深空探测技术专业委员会第九届学术年会论文集. 北京:CDSET,2012,1083-1091.
    [31] 陈罗婧,王沫,吕秋杰,等. 国外太阳帆薄膜材料选择及帆面展开方式研究进展[J]. 空间电子技术,2015(3):18-26. Chen L J,Wang M,Lv Q J,et al. Recent progress on solar sail membrane materials and deployment technology[J]. Space Electronic Technology,2015,3:18-26.
    [32] 刘金刚,倪洪江,高鸿,等. 超薄聚酰亚胺薄膜研究与应用进展,航天器环境工程[J]. 2014,31(5):470-475. Liu J G,Ni H J,Gao H,et al. Research and application of ultrathin polyimide films[J]. Space Environment Engineering,2014,31(5):470-475.
    [33] 沈自才,高鸿,牟永强. 空间近紫外辐照聚酰亚胺薄膜力学性能演化机理[J]. 真空科学与技术学报,2016,36(4):482-487. Chen Z C,Gao H,Mu Y Q,et al. Mechanism for changes in mechanical properties of polyimide membrane irradiated by near ultraviolet light[J]. Chinese Journal of Vacuum Science and Technology,2016,36(4):482-487.
    [34] 沈自才,郭亮,马子良,等. 聚酰亚胺薄膜在γ射线辐照下的力学性能退化研究[J]. 航天器环境工程,2016,33(1):100-104. Chen Z C,Guo L,Ma Z L,et al. Mechanical property degradation of polyimide film under gamma ray radiation[J]. Space Environment Engineering,2016,33(1):100-104.
    [35] Miura K,Natori M. 2-D Array experiment on bboard a space flyer unit[J]. Space Solar Power Review,1985,5(4):345-356.
    [36] Defocatiis D S A,Guest S D. Deployable membranes designed from folding tree leaves[J]. Philosophical Transaction of the Royal Society of London,Series A-Mathematical Physical and Engineering Sciences,2002,360(1791):227-238.
    [37] Melnikov V M,Koshelev V A. Large space structures formed by centrifugal Forces[J]. Earth Space Institute Book Series 4,Amsterdam:Gordon and Breach,1998,21-61.
    [38] Miyazaki Y,Shirasawa Y,Mori O,Sawada H. Finite element analysis of deployment of gossamer Space structure[C]//ECCOMAS Thematic Conference on Multibody Dynamics. Belgium:ECCOMAS,2011.
    [39] Murphy D M,Macy B D,Gaspar J L. Demonstration of a 10-m solar sail system[C]//Proceedings of the 46th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference.[S.l.]:AIAA,2004:AIAA 2004-1576.
    [40] Murphy D M,McEachen M E,Macy B D,Gaspar J L. Demonstration of a 20-m solar sail system[C]//Proceedings of the 46th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference.[S.l.]:AIAA,2005,AIAA-2005-2126.
    [41] Shirasawa Y,Mori O,Sawada H,Imaizumi T,et al. Demonstration of solar sail deployment system using a high altitude balloon[C]//Proceedings of The 27th International Symposium on Space Technology and Science.[S.l.]:[s.n.],2009,2009-d-36.
    [42] 黄小琦,王立,刘宇飞,杨辰等,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,2014,4:31-38. Huang X Q,Wang L,Liu Y F,et al. Numerical analysis on the deployment and folding process of large-scale solar sail membrane[J]. Chinese Space Science and Technology,2014,4:31-38.
    [43] 卫剑征,谭惠丰,马瑞强,宋博,充气式展开太阳帆结构动力学特性分析及展开试验[C]//西安:空间结构展开学术会议文集,2014,33.
    [44] 周晓俊,霍倩,周春燕,基于ADAMS的太阳帆展开绳索的建模与仿真[J]. 计算机辅助工程,2015,22(S1):194-197. Zhou X J,Huo Q,Zhou C Y. Modeling and simulation on solar sail deployment ropes based on Adams[J]. Computer Aided Engineering,2015,22(S1):194-197.
    [45] Liu C,Tian Q,Yan D,Hu H Y. Dynamic analysis of membrane systems undergoing overall motions,large deformations and wrinkles via thin shell elements of ANCF[J]. Computer Methods in Applied Mechanics and Engineering,2013,258(1):81-95.
    [46] Zhao J,Tian Q,Hu H Y. Deployment Dynamics of a simplified spinning IKAROS solar sail via Absolute Coordinate Based Method[J]. Acta Mechanica Sinica,2013,29(1):132-142.
    [47] 赵将,刘铖,田强,等. 粘弹性薄膜太阳帆自旋展开动力学分析[J]. 力学学报,2013,45(5):746-754. Zhao J,Liu C,Tian Q,et al. Dynamic analysis of spinning deployment of a solar sail composed of viscoelastic membranes[J]. Chinese Journal of Theoretical and Applied Mechanics,2013,45(5):746-754.
    [48] 周晓俊,周春燕,张兴新,等. 太阳帆自旋展开动力学地面模拟试验研究[J]. 振动工程学报,2015,28(2):175-182. Zhou X J,Zhou C Y,Zhang X X,et al. Ground simulation tests of spinning deployment dynamics of a solar sail[J]. Journal of Vibration Engineering,2015,28(2):175-182.
  • [1] 张宽, 于天一, 胡晓东, 刘传凯, 李立春, 赵焕洲.月面表层无人采样控制技术. 深空探测学报(中英文）, 2022, 9(2): 173-182.doi:10.15982/j.issn.2096-9287.2022.20210052
    [2] 薛鹏聪, 刘铖, 水小平.基于ANCF的薄膜太阳帆自旋展开动力学模拟. 深空探测学报(中英文）, 2022, 9(2): 217-229.doi:10.15982/j.issn.2096-9287.2022.20220004
    [3] 伊鑫, 潘豪, 黄聪, 胡海峰, 赵海滨.垂直回收运载火箭高精度姿态控制技术. 深空探测学报(中英文）, 2022, 9(5): 492-497.doi:10.15982/j.issn.2096-9287.2022.20210116
    [4] 王迎春, 王国欣, 赵帆, 张鼐, 王书超.深层月壤钻取冗余绕组电机控制方法. 深空探测学报(中英文）, 2021, 8(3): 259-268.doi:10.15982/j.issn.2096-9287.2021.20210014
    [5] 辛鹏飞, 吴跃民, 荣吉利, 危清清, 刘宾, 刘鑫.月面探测器圆形薄膜太阳翼展开动力学建模与分析. 深空探测学报(中英文）, 2020, 7(3): 255-263.doi:10.15982/j.issn.2095-7777.2020.20191128005
    [6] 杨洪伟, 宝音贺西.小行星附近制导与控制研究综述. 深空探测学报(中英文）, 2019, 6(2): 179-188.doi:10.15982/j.issn.2095-7777.2019.02.010
    [7] 王大轶, 符方舟, 孟林智, 李文博, 李茂登, 徐超, 葛东明.深空探测器自主控制技术综述. 深空探测学报(中英文）, 2019, 6(4): 317-327.doi:10.15982/j.issn.2095-7777.2019.04.002
    [8] 马传令, 刘勇, 梁伟光, 张尧.“嫦娥4号”中继星应急轨道控制策略设计与分析. 深空探测学报(中英文）, 2019, 6(3): 269-276.doi:10.15982/j.issn.2095-7777.2019.03.011
    [9] 陈莉丹, 谢剑锋, 刘勇, 陈明.中国深空探测任务轨道控制技术综述. 深空探测学报(中英文）, 2019, 6(3): 210-218.doi:10.15982/j.issn.2095-7777.2019.03.002
    [10] 李革非, 盛庆轩, 刘勇.基于交会模式的月球大椭圆轨道编队飞行控制. 深空探测学报(中英文）, 2019, 6(3): 261-268.doi:10.15982/j.issn.2095-7777.2019.03.010
    [11] 彭德云, 邹雪梅, 李亮.月球背面探测任务多目标协同控制模式设计. 深空探测学报(中英文）, 2018, 5(6): 544-553.doi:10.15982/j.issn.2095-7777.2018.06.007
    [12] 朱政帆, 高扬.空间小推力轨道最优Bang-Bang控制的两类延拓解法综述. 深空探测学报(中英文）, 2017, 4(2): 101-110.doi:10.15982/j.issn.2095-7777.2017.02.001
    [13] 徐彦, 郑耀, 匡松松, 周盛.展开式月球基地热防护结构方案研究. 深空探测学报(中英文）, 2016, 3(2): 168-174.doi:10.15982/j.issn.2095-7777.2016.02.012
    [14] 邬静云, 高有涛.利用绳系太阳帆减缓小行星自转的技术研究. 深空探测学报(中英文）, 2016, 3(1): 47-50.doi:10.15982/j.issn.2095-7777.2016.01.007
    [15] 江秀强, 陶婷, 杨威, 李爽.附着小天体的最优制导控制方法. 深空探测学报(中英文）, 2015, 2(1): 53-60.doi:10.15982/j.issn.2095-7777.2015.01.008
    [16] 武长青, 徐瑞, 朱圣英.基于对数势函数的深空探测器姿态规划与控制方法. 深空探测学报(中英文）, 2015, 2(4): 365-370.doi:10.15982/j.issn.2095-7777.2015.04.011
    [17] 曾祥远, 龚胜平, 李俊峰, 蒋方华, 宝音贺西.应用太阳帆悬停探测哑铃形小行星. 深空探测学报(中英文）, 2015, 2(1): 48-52.doi:10.15982/j.issn.2095-7777.2015.01.007
    [18] 郑燕红, 邓湘金, 赵志晖, 姚猛, 邹昕.月面回转钻进采样非脆弱鲁棒控制. 深空探测学报(中英文）, 2014, 1(4): 315-319.doi:10.15982/j.issn.2095-7777.2014.04.012
    [19] 贺晶, 龚胜平, 李俊峰.利用逃逸能量的太阳帆最快交会轨迹优化. 深空探测学报(中英文）, 2014, 1(1): 60-66.
    [20] 侯建文, 周杰.“火星科学实验室”巡航段导航、制导与控制. 深空探测学报(中英文）, 2014, 1(2): 110-116.
  • 加载中
WeChat 点击查看大图
计量
  • 文章访问数:2902
  • HTML全文浏览量:94
  • PDF下载量:1546
  • 被引次数:0
出版历程
  • 收稿日期:2016-09-01
  • 修回日期:2016-09-15

太阳帆航天器的关键技术

doi:10.15982/j.issn.2095-7777.2016.04.005
  • bob手机在线登陆宇航学院 飞行器动力学与控制教育部重点实验室, 北京 100081
  • 收稿日期:2016-09-01
  • 修回日期:2016-09-15

摘要:将太阳帆航天器所涉及的关键技术划分为4个方面：总体设计、轨道和姿态动力学与控制、太阳帆材料及其性能、太阳帆折叠与展开。针对每项关键技术，基于对国外长期研究结果进行分析并阐述主要技术特征，梳理国内相关研究进展，包括笔者与合作者的研究成果，分析存在的主要问题。根据上述分析，指出我国发展太阳帆航天器应该重视的若干问题。

English Abstract

胡海岩. 太阳帆航天器的关键技术[J]. 深空探测学报(中英文）, 2016, 3(4): 334-344. doi: 10.15982/j.issn.2095-7777.2016.04.005
引用本文: 胡海岩. 太阳帆航天器的关键技术[J]. 深空探测学报(中英文）, 2016, 3(4): 334-344.doi:10.15982/j.issn.2095-7777.2016.04.005
shu
HU Haiyan. Key Technologies of Solar Sail Spacecraft[J]. Journal of Deep Space Exploration, 2016, 3(4): 334-344. doi: 10.15982/j.issn.2095-7777.2016.04.005
Citation: HU Haiyan. Key Technologies of Solar Sail Spacecraft[J].Journal of Deep Space Exploration, 2016, 3(4): 334-344.doi:10.15982/j.issn.2095-7777.2016.04.005
shu

    全文HTML

参考文献 (48)

目录

    /

      返回文章
      返回

        您是第976321位访问者

        版权所有: 《深空探测学报》（中英文）编辑部编辑部地址: 中关村南大街5号邮编: 100081电话: （010）81384396/81384397

        本系统由北京仁和汇智信息技术有限公司开发 百度统计

        Baidu
        map