Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
Full-Text Search:
FQ: 双月
AD of Publication: 北京市
Lanuage: 英文;
ISSN: 1000-9361
CN: 11-1732/V
YP: 1988
Url: 中国航空学会;北京航空航天大学
Recommended Journals
2014 -01
A vision-based navigation approach with multiple radial shape marks for indoor aircraft locating Zhou Haoyin;Zhang Tao;Department of Automation,School of Information Science and Technology,Tsinghua University;National Key Laboratory of Integrated Flight Vehicle Control Technology,Xi'an Flight Automatic Control Research Institute;
Testability integrated evaluation method based on testability virtual test data Liu Guanjun;Zhao Chenxu;Qiu Jing;Zhang Yong;Science and Technology on Integrated Logistics Support Laboratory,National University of Defense Technology;
A salient edges detection algorithm of multi-sensor images and its rapid calculation based on PFCM kernel clustering Xu Guili;Zhao Yan;Guo Ruipeng;Wang Biao;Tian Yupeng;Li Kaiyu;College of Automation Engineering,Nanjing University of Aeronautics and Astronautics;
Weighted Marginal Fisher Analysis with Spatially Smooth for aircraft recognition Wei Zhenzhong;Liu Chang;Li Nan;Precision Opto-mechatrionics Technology,Key Laboratory of Education Ministry,Beihang University;
Description of shape characteristics through Fourier and wavelet analysis Yuan Zhanwei;Li Fuguo;Zhang Peng;Chen Bo;State Key Laboratory of Solidification Processing,Northwestern Polytechnical University;
Two-stage open-loop velocity compensating method applied to multi-mass elastic transmission system Zhang Deli;Yang Haiqiang;An Luling;College of Mechanical and Electrical Engineering,Nanjing University of Aeronautics and Astronautics;
Robust fault detection and optimization for a network of unmanned vehicles with imperfect communication channels Niu Erzhuo;Wang Qing;Dong Chaoyang;School of Automation Science and Electrical Engineering,Beihang University;School of Aeronautical Science and Engineering,Beihang University;
A strategic flight conflict avoidance approach based on a memetic algorithm Guan Xiangmin;Zhang Xuejun;Han Dong;Zhu Yanbo;Lv Ji;Su Jing;School of Electronic and Information Engineering,Beihang University;National Key Laboratory of CNS/ATM,Beihang University;Aviation Data Communication Corporation;
Precession–nutation correction for star tracker attitude measurement of STECE satellite Lai Yuwang;Liu Junhong;Ding Yonghe;Gu Defeng;Yi Dongyun;Department of Mathematics and Systems Science,National University of Defense Technology;Beijing Institute of Tracking and Telecommunication Technology;
Collision risk-capacity tradeoff analysis of an en-route corridor model Ye Bojia;Hu Minghua;John Friedrich Shortle;College of Civil Aviation,Nanjing University of Aeronautics and Astronautics;National Key Laboratory of Air Traffic Flow Management,Nanjing University of Aeronautics and Astronautics;Center for Air Transportation Systems Research,George Mason University;
Singular formalism and admissible control of spacecraft with rotating flexible solar array Lu Dongning;Liu Yiwu;Science and Technology on Intelligent Space Control Laboratory,Beijing Institute of Control Engineering;Beijing Institute of Control Engineering;
Sliding mode control based guidance law with impact angle constraint Zhao Yao;Sheng Yongzhi;Liu Xiangdong;School of Automation,Beijing Institute of Technology;Key Laboratory for Intelligent Control & Decision of Complex Systems,Beijing Institute of Technology;
Experimental study of partially-cured Z-pins reinforced foam core composites:K-Cor sandwich structures Zheng Yingying;Xiao Jun;Duan Mufeng;Li Yong;College of Materials Science and Technology,Nanjing University of Aeronautics and Astronautics;
Theoretical study of flow ripple for an aviation axial-piston pump with damping holes in the valve plate Guan Changbin;Jiao Zongxia;He Shouzhan;School of Automation Science and Engineering,Beihang University;Beijing Institute of Control Engineering;Science and Technology on Aircraft Control Laboratory,Beihang University;
Flutter analysis of an airfoil with nonlinear damping using equivalent linearization Chen Feixin;Liu Jike;Chen Yanmao;Department of Mechanics,Sun Yat-sen University;
Survey of orbital dynamics and control of space rendezvous Luo Yazhong;Zhang Jin;Tang Guojin;College of Aerospace Science and Technology,National University of Defense Technology;
Recent advance in nonlinear aeroelastic analysis and control of the aircraft Xiang Jinwu;Yan Yongju;Li Daochun;School of Aeronautic Science and Engineering,Beihang University;
Acoustic measurements of models of military style supersonic nozzle jets Ching-Wen Kuo;Jérémy Veltin;Dennis K.McLaughlin;Department of Aerospace Engineering,The Pennsylvania State University,University Park;TNO Science and Industry;
Generalized Kutta–Joukowski theorem for multi-vortex and multi-airfoil flow(a lumped vortex model) Bai Chenyuan;Wu Ziniu;School of Aerospace,Tsinghua University;
A spongy icing model for aircraft icing Li Xin;Bai Junqing;Hua Jun;Wang Kun;Zhang Yang;School of Aerodynamics,Northwestern Polytechnical University;Chinese Aeronautical Establishment;
Multi-objective optimization of aircraft design for emission and cost reductions Wang Yu;Yin Hailian;Zhang Shuai;Yu Xiongqing;Key Laboratory of Fundamental Science for National Defense,Advanced Design Technology of Flight Vehicle,Nanjing University of Aeronautics and Astronautics;
2014 Issues:  [01] [02] [03] [04] [05] [06]
More Issues:   [1994]   [1995]   [1996]   [1997]   [1998]   [1999]   [2000]   [2001]   [2002]   [2003]   [2004]   [2005]   [2006]   [2007]   [2008]   [2009]   [2010]   [2011]   [2012]   [2013]   [2015]   [2016]   [2017]   [2018]
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved