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Uncertainty analysis and probabilistic design optimization of hybrid rocket motors for manned lunar landing
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science china(Technological sciences)》2015年 第7期58卷 1234-1241页
作者:ZHU Hao TIAN Hui CAI GuoBiao BAO WeiMinSchool of Astronautics Beihang University China Aerospace Science and Technology Corporation 
To obtain a conceptual design for a hybrid rocket motor(HRM)to be used as the Ascent Propulsion System in the Apollo lunar module,the deterministic design optimization(DDO)method is applied to the HRM *** on the resul...
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背应力平衡策略实现非均质Al-SiC复合材料的强塑性协同
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science china Materials》2023年 第4期66卷 1649-1658页
作者:冒冬鑫 孟祥晨 谢聿铭 常月鑫 秦志伟 许双明 万龙 黄永宪State Key Laboratory of Advanced Welding and JoiningHarbin Institute of TechnologyHarbin 150001China Zhengzhou Research InstituteHarbin Institute of TechnologyZhengzhou 450000China China Aerospace Science and Technology CorporationBeijing 100000China 
高强复合材料的低位错存储性能及其引发的强塑倒置问题阻碍了该系列材料的进一步发展.本文通过新颖的形变驱动冶金方法,设计了一种巧妙的具有粗细晶粒异质结构的纳微混合SiC增强铝基复合材料.基于背应力理论对累积的几何必须位错和晶内...
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A new robust design for imperfection sensitive stiffened cylinders used in aerospace engineering
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science china(Technological sciences)》2015年 第5期58卷 796-802页
作者:LIANG Ke ZHANG YongJie SUN Qin RUESS MartinSchool of Aeronautics Northwestern Polytechnical University Qian Xuesen Laboratory of Space Technology China Aerospace Science and Technology Corporation Faculty of Aerospace Engineering Delft University of Technology 
A knock-down factor is commonly used to take into account the obvious decline of the buckling load in a cylindrical shell caused by the inevitable imperfections. In 1968, NASA guideline SP-8007 gave knock-down factors...
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Conformal optical design with combination of static and dynamic aberration corrections
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《Chinese Physics B》2009年 第2期18卷 565-570页
作者:李岩 李林 黄一帆 刘家国Department of Optoelectronic Engineering Beijing Institute of Technology 207 Institute of China Aerospace Science & Industry Corporation 50 Yongding Road Haidian District 
Conformal domes that are shaped to meet aerodynamic requirements can increase range and speed for the host platform. Because these domes typically deviate greatly from spherical surface descriptions, a variety of aber...
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Cooperative Guidance Law Design for Simultaneous Attack with Multiple Missiles Against a Maneuvering Target
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《Journal of Systems science & Complexity》2018年 第1期31卷 287-301页
作者:ZHOU Jialing Lü Yuezu LI Zhongkui YANG JianyingMinisterial Key Laboratory of ZNDY School of Mechanical Engineering Nanjing University of Science and Technology Nanjing 210094 China National Defense Key Laboratory of Science and Technology on Electromagnetic Scattering the 802 Institute of Shanghai Academy of Space Flight Technology the Eighth Academy of China Aerospace Science and Technology Corporation Shanghai 200090 China State Key Laboratory for Turbulence and Complex Systems Department of Mechanics and Engineering Science College of Engineering Peking University Beijing 100871 China 
这份报纸对一个调遣的目标考虑多重导弹的同时的攻击问题。与大多数同时的攻击问题在被提出的存在文学不同当导弹 time-to-go 的一个一致问题估计,这份报纸作为导弹 ranges-to-go 的一致问题提出它。基于这策略,新奇分布式的指导法律...
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基于综合集成研讨厅的群体智能设计研究(英文)
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《Frontiers of Information technology & Electronic Engineering》2017年 第1期18卷 149-152页
作者:Bo-hu LI Hui-yang QU Ting-yu LIN Bao-cun HOU Xiang ZHAI Guo-qiang SHI Jun-hua ZHOU Chao RUANThe Second Academy of China Aerospace Science and Technology Corporation The State Key Laboratory of Intelligent Manufacturing System for Complex Products Beijing Aerospace Intelligent Manufacturing Technology Development Co.Ltd. 
本文提出了一种基于综合集成研讨厅的群体智能设计技术,包括系统的体系架构、基于综合集成研讨的设计决策过程以及设计资源推送技术,最后在对本文工作进行总结的基础上,对下一步研究方向进行了展望。
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