Kinematic and mechanical analysis on launch process of stratospheric airship

被引：0
|
作者：
Zhang T. [1 ,2 ]
Jiang L. [1 ,3 ]
Zhou J. [1 ]
机构：
[1] Academy of Opto-Electronics, Chinese Academy of Sciences, Beijing
[2] University of Chinese Academy of Sciences, Beijing
[3] Institute of High Energy Physics, Chinese Academy of Sciences, Beijing
来源：
Jiang, Luhua (jianglh@ihep.ac.cn) | 2018年 / Beijing University of Aeronautics and Astronautics (BUAA)卷 / 44期
关键词：
Dynamics analysis; Launch process; Multi-helium envelope structure; Single helium envelope structure; Stratospheric airship;
D O I：
10.13700/j.bh.1001-5965.2017.0227
中图分类号：
学科分类号：
摘要：
Launch mode of the stratospheric airship is the prerequisite factor to safely reach the target altitude. In this paper, a dynamics model for the launch process of stratospheric airship is firstly established, and the analytical solution method is put forward, and the quantitative analysis is carried out. Secondly, according to the typical issues that influence the launch process, the dynamic analysis of both the single-helium and multi-helium envelope structure are carried out, including dynamics response and force status. Furthermore, the numerical results of a single helium envelope structure are obtained and then compared with experimental data. The result verified the accuracy of the analytical method, which can also provide the basis for launch process of the airship and the design of the launch equipment. © 2018, Editorial Board of JBUAA. All right reserved.
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页码：691 / 699
页数：8
相关论文
共 19 条
  • [1] Liao L., Pasternak I., A review of airship structural research and development, Progress in Aerospace Sciences, 45, 4-5, pp. 83-96, (2009)
  • [2] Stockbridge C., Ceruti A., Marzocca P., Airship research and development in the areas of design, structures, dynamics and energy systems, International Journal of Aeronautical & Space Sciences, 13, 2, pp. 170-187, (2012)
  • [3] Wilson J.R., A new era for airships, Aerospace America, 42, 5, pp. 27-31, (2004)
  • [4] Steve S., The HiSentinel airship, 7th AIAA Aviation Technology, Integration and Operations Conference, (2007)
  • [5] Smith I., Lee M., Fortneberry M., Et al., HiSentinel80: Flight of a high altitude airship, 11th AIAA Aviation Technology, Integration, and Operations Conference, (2011)
  • [6] Lockheed Martin Space System Company High altitude airship
  • [7] Future aerostat and airship investment decisions drive oversight and coordination needs: GAO-13-81, (2012)
  • [8] Ground-to-stratosphere flight test and evaluation of materials and structure for stratospheric airship test vehicle: JAXA-RM-04-012, pp. 7-35, (2004)
  • [9] Shunichi O., Noboru S., R&D status of RFC technology for SPF airship in Japan, 9th Annual International Energy Conversion Engineering Conference, (2011)
  • [10] Selby C., High altitude airship station keeping and launch model development using output from numerical weather prediction models, (2008)
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