ZHAO Da , LIU Dongxu , SUN Kangwen , TAO Guoquan , ZHU Ming , WU Zhe . Research status, technical difficulties and development trend of stratospheric airship[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016 , 37(1) : 45 -56 . DOI: 10.7527/S1000-6893.2015.0332

[1] MASAHIKO O.Design and applications of a stratospheric long endurance LTA platform:AIAA-2001-5266[R].Reston:AIAA,2001.
[2] CATHEY H M.The NASA super pressure balloon-A path to flight[J].Advances in Space Research,2009,44(1):23-38.
[3] SMITH S,RAINWATER E L.Applications of scientific ballooning technology to high altitude airships[C]//Proceedings of AIAA's 3rd Annual Aviation Technology,Intergration,and Operations Tech.Reston:AIAA,2003:1-8.
[4] LARDIONIS F.Google X announces project loon:Balloon-powered Internet for rural,remote and underserved areas[EB/OL].2013.(2013-06-14) [2015-11-03].http://techcrunch.com/2013/06/14/google-x-announces-project-loon-balloon-powered-internet-for-rural-remote-and-underserved-areas.html.
[5] YOUNG M.An overview of advanced concepts fornear-space systems:AIAA-2009-4805[R].Reston:AIAA,2009.
[6] SCHMIDT D K,STEVENS J,RONEY J.Near-space station-keeping performance of a large high-altitude notional airship[J].Journal of Aircraft,2007,44(2):611-615.
[7] GABRIEL A,KHOURY J,DAVID G.Airship technology[M].London:Cambridge University Press,1999:327-351.
[8] 昌敏,周洲,王睿.基于机翼-帆尾的高纬度跨年驻留太阳能飞机总体参数设计方法[J].航空学报,2014,35(6):1592-1603.CHANG M,ZHOU Z,WANG R.Primary parameters determination for year-round solar-powered aircraft of wing-sail type at higher latitudes[J].Acta Aeronautica et Astronautica Sinica,2014,35(6):1592-1603(in Chinese).
[9] 李利良,郭伟民,何家芳.国外近空间飞艇的现状和发展[J].武器装备自动化,2008,27(2):32-35.LI L L,GUO W M,HE J F.Current situation and development of foreign near space airship[J].Armament Automation,2008,27(2):32-35(in Chinese).
[10] 姚伟,李勇,王文隽,等.美国平流层飞艇发展计划和研究进展[J].航天器工程,2008,17(2):69-75.YAO W,LI Y,WANG W J,et al.Development plan and research progress of stratospheric airship in USA[J].Spacecraft Engineering,2008,17(2):69-75(in Chinese).
[11] ANDROULAKAKIS S P,JUDY R A.Status and plans of high altitude airship(HAATM) program[C]//Proceedings of AIAA Lighter-Than-Air Systems Technology(LTA) Conference.Reston:AIAA,2013:25-28.
[12] 曹旭,顾正铭,王伟志,等.美国ISIS平流层飞艇概述[C]//2011年中国浮空器大会论文集.北京:航空工业出版社,2011:114-119.CAO X,GU Z M,WANG W Z,et al.The review of USA ISIS stratospheric airship[C]//Proceedings of 2011 China Aviation Society and Aerostat Research Conference.Beijing:Aviation Industry Press,2011:114-119(in Chinese).
[13] SMITH S,FORTENBERRY M,LEE M,et al.HiSentinel80:Flight of a high altitude airship[C]//Proceedings of the 11th AIAA Aviation Technology,Integration,and Operations(ATIO) Conference.Reston:AIAA,2011:1-14.
[14] KIESSLING A,DIAZ E,MILLER S,et al.The 20-20-20 airship challenge[C]//Proceedings of American Astronomical Society Meeting.Washington,D.C.:American Astronomical Society,2014:224.
[15] OKAYA S,SHINOZAKI N,SASA S,et al.R & D status of RFC technology for SPF airship in Japan:AIAA-2011-5896[R].Reston:AIAA,2011.
[16] GRACE D,MOHORCIC M,OODO M,et al.CAPANINA-communications from aerial platform networks delivering broadband information for all[C]//Proceedings of the 14th IST Mobile and Wireless and Communications Summit.Dresden,Germany:IST Summit,2005.
[17] CHESSEL J P.Stratobus-The autonomous,stationary,stratospheric platform[EB/OL].(2015-05-22) [2015-11-03].https://www.thalesgroup.com/en/worldwide/space/magazine/space-qa-all-about-stratobus.
[18] 中国科学院.平流层试验飞艇飞行试验圆满成功[EB/OL].(2012-09-04) [2015-11-03].http://www.antpedia.com/news/85/n-239085.html.Chinese Academy of Sciences.The success of stratospheric test airship flight test[EB/OL].(2012-09-04) [2015-11-03].http://www.antpedia.com/news/85/n-239085.html(in Chinese).
[19] 中国航天科工集团公司.国产平流层浮空器飞行试验取得成功[EB/OL].(2015-08-16) [2015-11-03].http://www.sasac.gov.cn/n86114/n326638/c2030709/content.html?from=groupmessage&isappinstalled=0.China Aerospace Science and Industry Corporation.The success of domestic stratospheric aerostat flight test[EB/OL].(2015-08-16) [2015-11-03].http://www.sasac.gov.cn/n86114/n326638/c2030709/content.html?from=groupmessage&isappinstalled=0(in Chinese).
[20] 赵沐阳.上海交通大学低速临近空间飞行器飞行试验圆满成功[EB/OL].(2015-10-10) [2015-11-03].http://kejichu.sjtu.edu.cn/info/1009/62129.htm.ZHAO M Y.The low speed near space flight test of Shanghai Jiao Tong University is a complete success[EB/OL].(2015-10-10) [2015-11-03].http://kejichu.sjtu.edu.cn/info/1009/62129.htm(in Chinese).
[21] 王海峰,宋笔锋,刘斌,等.高空飞艇总体设计方法研究[J].西北工业大学学报,2007,25(1):56-60.WANG H F,SONG B F,LIU B,et al.Exploring configuration design of high altitude airship[J].Journal of Northwestern Polytechnical University,2007,25(1):56-60(in Chinese).
[22] 施红,宋保银,姚秋萍,等.平流层飞艇太阳能源系统研究[J].中国空间科学技术,2009,29(1):26-31.SHI H,SONG B Y,YAO Q P,et al.Study of the solar power system of stratospheric airships[J].Chinese Space Science and Technology,2009,29(1):26-31(in Chinese).
[23] HULL D G.Conversion of optimal control problems into parameter optimization problems[J].Journal of Guidance,Control,and Dynamics,1997,20(1):57-60.
[24] 李智斌,张芸香,倪茂林,等.平流层飞艇控制与推进技术[J].航天控制,2007,25(1):21-25.LI Z B,ZHANG Y X,NI M L,et al.Control and propulsion technology of stratosphere airships[J].Aerospace Control,2007,25(1):21-25(in Chinese).
[25] MAEKAWA S,SHIBASAKI K,KUROSE T,et al.Tear propagation of a high-performance airship envelope material[J].Journal of Aircraft,2008,45(5):1546-1553.
[26] 郝佳傲,蒋崇文,高振勋,等.国外平流层飞艇气动布局设计研究进展分析[J].飞航导弹,2013(11):53-59.HAO J A,JIANG C W,GAO Z X,et al.Headway of foreign research about aerodynamic configuration of near-space airship[J].Aerodynamic Missile Journal,2013(11):53-59(in Chinese).
[27] 麻震宇,侯中喜,杨希祥,等.临近空间大型柔性充气囊体结构特性分析[J].国防科技大学学报,2015,37(4):25-30.MA Z Y,HOU Z X,YANG X X,et al.Structural performance analysis of large-scale flexible inflatable structures for stratospheric airships[J].Journal of National University of Defense Technology,2015,37(4):25-30(in Chinese).
[28] 甘晓华,郭颍.飞艇技术概论[M].北京:国防工业出版社,2005:49-52.GAN X H,GUO Y.Introduction to airship technology[M].Beijing:National Defense Industry Press,2005:49-52(in Chinese).
[29] KORNMANN R,KROPLIN B,EPPERLEIN F.Flight tests of a remote controlled model of an LTA vehicle based on a new airship concept,the airworm principle[R].Stuttgart,Germany:Institute for Statics and Dynamics of Aerospace Structures,Stuttgart University,2001.
[30] 李晓阳.变体飞艇创新技术及其科学意义[J].前沿科学,2008,2(2):53-62.LI X Y.The innovatory technology of transformable airship and its scientific significance[J].Frontier Science,2008,2(2):53-62(in Chinese).
[31] 任一鹏,田中伟,吴子牛,等.飞艇空气动力学及其相关问题[J].航空学报,2010,31(3):431-443.REN Y P,TIAN Z W,WU Z N,et al.Some aerodynamics problems of airship[J].Acta Aeronautica et Astronautica Sinica,2010,31(3):431-443(in Chinese).
[32] 谭惠丰,刘羽熙,刘宇艳,等.平流层飞艇蒙皮材料研究进展和需求分析[J].复合材料学报,2012,29(6):1-8.TAN H F,LIU Y X,LIU Y Y,et al.Research progress and requirement analysis of envelope materials for near space airship[J].Acta Materiae Compositae Sinica,2012,29(6):1-8(in Chinese).
[33] SAID M A,DINGWALL B,GUPTA A,et al.Investigation of ultra violet(UV) resistance for high strength fibers[J].Advances in Space Research,2006,37(11):2052-2058.
[34] KOMATSU K,SANO M,KAKUTA Y.Development of high specific strength envelope materials[C]//Proceedings of AIAA's 3rd Annual Aviation Technology,Intergration,and Operations Tech.Reston:AIAA,2003.
[35] 赵臻璐,王小群,杜善义,等.平流层飞艇囊体气密层材料及氦气透过聚合物研究现状[J].航空学报,2009,30(9):1761-1768.ZHAO Z L,WANG X Q,DU S Y,et al.Review of research on gas retention layer material for stratospheric airship envelope and helium permeation in polymers[J].Acta Aeronautica et Astronautica Sinica,2009,30(9):1761-1768(in Chinese).
[36] 刘山生,李洁涛.GB/T 1038-2000 塑料薄膜和薄片气体透过性试验方法-压差法[S].北京:国家质量技术监督局,2000.LIU S S,LI J T.GB/T 1038-2000 Plastics-film and sheeting-determination of gas transmission-differential-pressure method[S].Beijing:General Administration of Qultity Supervision,Inspection and Quanantine of the People's Republic of China,2000(in Chinese).
[37] 王涛,钱斌,杨洋.平流层飞艇能源系统进展与展望[C]//2015平流层飞艇技术研讨会议文集.北京:中国航空学会浮空器分会,2015.WANG T,QIAN B,YANG Y.The progress and prospect of stratospheric airship energy system[C]//Proceedings of 2015 Stratospheric airship Technology Research Conference.Beijing:China Aviation Society and Aerostat Branch,2015(in Chinese).
[38] 刘勇.国外平流层飞艇用电源技术进展[J].电源技术,2011,35(12):1617-1618.LIU Y.Review of power source for oversea stratospheric airship[J].Chinese Journal of Power Sources,2011,35(12):1617-1618(in Chinese).
[39] 宋世栋,张华民,马霄平,等.一体式可再生燃料电池[J].化学进展,2006,18(10):1375-1380.SONG S D,ZHANG H M,MA X P,et al.Unitized regenerative fuel cells[J].Progress in Chemistry,2006,18(10):1375-1380(in Chinese).
[40] 陈宋,孙凤焕,张明,等.可再生燃料电池系统在空间电源中的应用研究[J].航天器工程,2014,23(6):128-134.CHEN S,SUN F H,ZHANG M,et al.Application analysis of regenerative fuel cell system in space electrical power[J].Spacecraft Engineering,2014,23(6):128-134(in Chinese).
[41] 方丽娟,屈卫东.平流层飞艇多能源的优化管理系统[J].控制工程,2008,15(S0):172-175.FANG L J,QU W D.Optimization management system of multi-energy control in stratosphere airship[J].Control Engineering of China,2008,15(S0):172-175(in Chinese).
[42] 李智斌,吴雷,张景瑞,等.平流层飞艇动力学与控制研究进展[J].力学进展,2012,42(4):482-493.LI Z B,WU L,ZHANG J R,et al.Review of dynamics and control of stratospheric airship[J].Advances in Mechanics,2012,42(4):482-493(in Chinese).
[43] 刘丹,王晓亮,单雪雄.平流层飞艇的附加质量及其对飞艇运动的影响[J].计算机仿真,2006,23(6):52-56 .LIU D,WANG X L,SHAN X X.Added mass to stratospheric airship and it s effect on motion[J].Computer Simulation,2006,23(6):52-56(in Chinese).
[44] 王海峰,宋笔锋,王海平.高空飞艇定点控制关键技术及解决途径[J].飞行力学,2005,23(4):5-8.WANG H F,SONG B F,WANG H P.The key technology and solution of fixed point control of high altitude airship[J].Flight Dynamics,2005,23(4):5-8(in Chinese).
[45] 王明建,刘国辉,魏峰,等.滑模变结构控制在平流层飞艇姿态控制中的应用[J].电光与控制,2010,17(6):65-68.WANG M J,LIU G H,WEI F,et al.Application of variable-structure control with sliding mode in attitude control of stratospheric airships[J].Electronics Optics & Control,2010,17(6):65-68(in Chinese).
[46] 郭建国,周军.基于滑模神经网络的自主飞艇姿态控制[J].飞行力学,2009,27(1):40-42.GUO J G,ZHOU J,Control system of autonomous airship based on siding mode control and neural network[J].Flight Dynamics,2009,27(1):40-42(in Chinese).
[47] 张守旭,严卫生,谢兰,等.非线性PID控制技术在飞艇上的应用[J].电子设计工程,2014,22(7):64-66.ZHANG S X,YAN W S,XIE L,et al.Nonlinear PID control technology applied to the airship[J].Electronic Design Engineering,2014,22(7):64-66(in Chinese).
[48] 郭建国,周军.临近空间低动态飞行器控制研究综述[J].航空学报,2014,35(2):320-331.GUO J G,ZHOU J.Review of the control of low dynamic vehicles in near space[J].Acta Aeronautica et Astronautica Sinica,2014,35(2):320-331(in Chinese).
[49] 孟蒙.基于热力学模型的平流层飞艇升降过程复合控制[D].上海:上海交通大学,2013.MENG M,Compound control for ascending and descending of stratospheric airship with thermal model[D].Shanghai:Shanghai Jiao Tong University,2013(in Chinese).
[50] 孙帅,李智斌,田科丰.考虑风场条件的一类平流层飞艇返回过程建模与航迹规划研究[J].空间控制技术与应用,2014,40(4):37-41.SUN S,LI Z B,TIAN K F.Modeling and trajectory planning of return process for a class of airship with wind field[J].Aerospace Control and Application,2014,40(4):37-41(in Chinese).
[51] 胡国昌,夏辉,吴美平.平流层飞艇静升力分析[J].计算机仿真,2010,27(12):60-64.HU G C,XIA H,WU M P.Analysis on static lift of stratospheric airship[J].Computer Simulation,2010,27(12):60-64(in Chinese).
[52] 赵攀峰,王永林,刘传超,等.平流层飞艇放飞、回收过程初步分析[J].航空科学技术,2007(4):25-30.ZHAO P F,WANG Y L,LIU C C,et al.Preparatory analyse on the release and recovery course of stratosphere airship[J].Aeronautical Science and Technology,2007(4):25-30(in Chinese).
[53] JOSEPH M,YIYUAN Z,WILLIAM G.Optimal ascent trajectories for stratospheric airships using wind energy[J].Journal of Guidance,Control,and Dynamics,2009,32(4):1232-1245.
[54] 彭桂林,吴晴.飞艇平台推力矢量转向系统的设计[J].机械传动,2011,35(10):13-15.PENG G L,WU Q.Design of thrust vector steering mechanism for airship platform[J].Journal of Mechanical Transmission,2011,35(10):13-15(in Chinese).
[55] 罗玲,刘卫国,窦满峰,等.高空飞艇螺旋桨驱动电机分析[J].宇航学报,2009,30(6):2140-2144.LUO L,LIU W G,DOU M F,et al.Analysis of the motor driving a propeller of high altitude airship[J].Journal of Astronautics,2009,30(6):2140-2144(in Chinese).