| [1] Zhao Z L, Wang X Q, Du S Y. Review of research on gas retention layer material for stratospheric airship envelope and helium permeation in polymers.Acta Aeronautica et Astronautica Sinica,2009,30(9): 1761-1767. (in Chinese) 赵臻璐, 王小群, 杜善义. 平流层飞艇囊体气密层材料及氦气透过聚合物研究现状. 航空学报, 2009, 30(9): 1761-1767.[2] Khoury G A, Gillett J D. Airship technology. Cambridge: Cambridge University Press, 1999: 1-10.[3] Zhu Y C, Chang W J, Fu Y. Environmental suitability of weapons and environmental engineering. Equipment Environmental Engineering, 2005, 2(1): 14-19. (in Chinese) 祝耀昌, 常文君, 傅耘. 武器装备环境适应性与环境工程. 装备环境工程, 2005, 2(1): 14-19.[4] Li S L, Yang S, Sun D. Evaluation model of environmental worthiness for military aircraft. Acta Aeronautica et Astronautica Sinica, 2009,30(6): 1053-1057. (in Chinese) 李曙林, 杨森, 孙冬. 军用飞机环境适应性评价模型. 航空学报, 2009, 30(6): 1053-1057.[5] Qu X Y, Deng L. Analysis of the environmental worthiness of shipborne weapons in marine environment. Ship Electronic Engineering, 2011, 31(4): 138-146. (in Chinese) 曲晓燕, 邓力. 舰载武器海洋环境适应性分析. 舰船电子工程, 2011, 31(4): 138-146.[6] Anthony C. Initial feasibility assessment of a high altitude long endurance airship. NASA CR-212724, 2003.[7] Chen Q, Zhu M, Sun K W. Analysis to effects on conceptual parameters of stratospheric airship with specified factors. Journal of Computers, 2011, 6(5): 1055-1062.[8] Joseph B M, Zhao Y Y, William L G. Optimal ascent trajectories for stratospheric airships using wind energy. Journal of Guidance Control and Dynamics, 2009, 32(9): 1232-1245.[9] David K S, James S, Jason R. Near-space station keeping performance of a large high-altitude notional airship. Journal of Aircraft, 2007, 44(2): 611-615.[10] Ma W, Xuan Y M, Han Y G. Thermal environment analysis and thermal design principle of stratospheric vehicles. Journal of Astronautic, 2010, 31(5): 1272-1277. (in Chinese) 马伟, 宣益民, 韩玉阁. 临近空间热环境分析及低速飞行器的热设计方法. 宇航学报, 2010, 31(5): 1272-1277.[11] Yang B, Yang J. Analysis of the operating environment of near-space airship and its effects. 2008 Aerostat Conference Proceeding. Beijing: Institute of Electronics, Chinese Academy of Sciences, 2008: 395-398. (in Chinese) 杨秉, 杨健. 临近空间飞艇运行环境及其影响分析. 2008年中国浮空器大会论文集. 北京: 中国科学电子学研究所, 2008: 395-398.[12] Yao W, Li Y, Zheng W, et al. Analysis of flight temperature limits and flight velocity limits for stratospheric airship. Journal of Astronautic, 2011, 32(6): 1239-1243. (in Chinese) 姚伟, 李勇, 郑威, 等. 平流层飞艇飞行温度限和飞行速度限分析. 宇航学报, 2011, 32(6): 1239-1243.[13] Zhang Z Q, Xu B, He Y L, et al. Engine performance evaluation based on analytic hierarchy process.Acta Armamentari, 2008, 29(5): 625-628.(in Chinese) 张志强, 徐斌, 何勇灵, 等. 基于AHP评价方法的发动机性能评价. 兵工学报, 2008, 29(5): 625-628.[14] Chen Y, Chen X K, Lin Y. Application of improved radar chart evaluation method on evaluation of automobile comprehensive performances. Journal of Jilin University, 2011, 41(6): 1522-1526. (in Chinese) 陈勇, 陈潇凯, 林逸. 改进雷达图评价方法在汽车综合性能评价中的应用. 吉林大学学报, 2011, 41(6): 1522-1526.[15] Xue L H, Huang H Z, Zhang X, et al. Study of model for linear physical programming-based evaluation and decision-making of conceptual design schemes. Journal of Dalian University of Technology, 2005, 45(4): 562-567. (in Chinese) 薛立华, 黄洪钟, 张旭, 等. 概念设计方案评价和决策线性物理规划模型研究. 大连理工大学学报, 2005, 45(4): 562-567.[16] Wang Y L, Li W J. Physical programming and its application in aircraft concept design. Acta Aeronautica et Astronautica Sinica, 2005, 26(5): 562-566. (in Chinese) 王允良, 李为吉. 物理规划方法及其在飞机方案设计中的应用. 航空学报, 2005, 26(5): 562-566. |
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