中国科学院机构知识库网格
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浏览/检索结果: 共8条,第1-8条 帮助

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Unusual Phase Transition of Poly(di(alkyl) vinylterephthalates) 期刊论文  OAI收割
ACTA POLYMERICA SINICA, 2017, 期号: 9, 页码: 1506-1516
作者:  
Liu, Xin;  Zheng, Xiao-hui;  Liu, Xiao-qing;  Zhao, Rui-ying;  Zhao, Ti-peng
  |  收藏  |  浏览/下载:43/0  |  提交时间:2018/04/25
Normal acceleration reduce guidanceand control for sub-orbit vehicle re-entry 会议论文  OAI收割
Xiamen, China, 6-9 March 2017
作者:  
Li WH(李文皓);  Xiao XX(肖歆昕);  Zhang H(张珩);  Xiao XX(肖歆昕)
收藏  |  浏览/下载:34/0  |  提交时间:2018/01/16
Time-varying Spectrum Based Active Disturbance Rejection Control for Hypersonic Reentry Vehicle 会议论文  OAI收割
Harbin, China, August 7-10, 2016
作者:  
Zhiqiang Pu;  Jianhong Zhang;  Ruyi Yuan;  Jianqiang Yi
  |  收藏  |  浏览/下载:29/0  |  提交时间:2016/10/25
An integrated composite with a porous C-f/C-ZrB2-SiC core between two compact outer layers of C-f/C-ZrB2-SiC and C-f/C-SiC 期刊论文  OAI收割
Journal of the European Ceramic Society, 2015, 卷号: 35, 期号: 3, 页码: 1113-1117
C. L.; Pang Hu, S. Y.; Tang, S. F.; Wang, Y. C.; Cheng, H. M.
收藏  |  浏览/下载:31/0  |  提交时间:2015/05/08
The role of epigenomics in the neurodegeneration of ataxia-telangiectasia 期刊论文  OAI收割
EPIGENOMICS, 2015, 卷号: 7, 期号: 2, 页码: 137-141
作者:  
Li JL[*];  Jiang DW
收藏  |  浏览/下载:25/0  |  提交时间:2015/07/07
Reentry guidance based on parametric optimization (EI CONFERENCE) 会议论文  OAI收割
2012 International Conference on Mechatronics and Control Engineering, ICMCE 2012, November 29, 2012 - November 30, 2012, Guangzhou, China
作者:  
Li D.
收藏  |  浏览/下载:168/0  |  提交时间:2013/03/25
Reentry guidance based on feedback linearization (EI CONFERENCE) 会议论文  OAI收割
2011 International Conference on Electronics, Communications and Control, ICECC 2011, September 9, 2011 - September 11, 2011, Ningbo, China
Li D.-W.
收藏  |  浏览/下载:31/0  |  提交时间:2013/03/25
This paper presents a new reentry guidance algorithm for RLV (Reusable Launching Vehicle). The algorithm consists of two integrated components: trajectory planning algorithm and tracking algorithm. The most striking feature of algorithm here lies in that both planning and tracking are executed directly in height-velocity space  which is different from the methodology of configuration of drag in traditional shuttle guidance. In the session of trajectory planning  all trajectory constraints can be expressed with upper bound and lower bound in height-velocity space  then a linear interpolation is carried to search the nominal trajectory satisfying the requirement of downrange and target constraints. Then the tracking algorithm uses feedback linearization method to track this nominal profile and meet all constraints. Another typical feature of this algorithm is the strategy of downrange extension using FPA (flight path angle) controller to fulfill the requirement of large downrange. Proper combination of planning-tracking algorithm and FPA controller can bring great flexibility and adaptability to reentry guidance. The algorithm is proved to be robust enough to accommodate the model error and noises in the dynamics. 2011 IEEE.  
再入尾迹电磁特性的湍流效应研究 学位论文  OAI收割
博士, 北京: 中国科学院研究生院, 2000
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收藏  |  浏览/下载:1132/95  |  提交时间:2009/04/13