1001-5965
2014 Issue 4
Influencing depth under aircraft loads of runway
Zhang Xianmin;Xue Huaxin;Dong Qian;Sun Zhichao;Airport College;Civil Aviation University of China;
Zhang Xianmin;Xue Huaxin;Dong Qian;Sun Zhichao;Airport College;Civil Aviation University of China;
..............page:427-432
Influence of frequency mixing on vibration test of fiber optic gyroscope
Song Ningfang;Zhao Yafei;Pan Xiong;Zhang Chunsheng;School of Instrumentation Science and Opto-electronics Engineering;Beijing University of Aeronautics and Astronautics;
Song Ningfang;Zhao Yafei;Pan Xiong;Zhang Chunsheng;School of Instrumentation Science and Opto-electronics Engineering;Beijing University of Aeronautics and Astronautics;
..............page:433-438
Numerical simulation analysis of steady-state properties of gas face and cylinder film seal
Ma Gang;Sun Xiaojun;Luo Xianhai;He Jun;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;
Ma Gang;Sun Xiaojun;Luo Xianhai;He Jun;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;
..............page:439-443
Influence of laser shock peening times on microstructure and hardness of TA15 titanium alloy
Zhu Ying;Fan Bowen;Guo Wei;Kang Hui;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;
Zhu Ying;Fan Bowen;Guo Wei;Kang Hui;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;
..............page:444-448
Decoupling PI controller design for aeroengine
Gao Yahui;Zang Jun;Yao Hua;Huang Jinquan;AVIC China Aviation Motor Control System Institute;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
Gao Yahui;Zang Jun;Yao Hua;Huang Jinquan;AVIC China Aviation Motor Control System Institute;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:449-454
Loop parameters on dynamic characteristics of digital closed-loop accelerometer
Zhang Xi;Zhang Shengyan;Li Lijing;Wang Hongbo;School of Instrumentation Science and Opto-electronics Engineering;Beijing University of Aeronautics and Astronautics;Shanghai Institute of Spaceflight Control Technology;
Zhang Xi;Zhang Shengyan;Li Lijing;Wang Hongbo;School of Instrumentation Science and Opto-electronics Engineering;Beijing University of Aeronautics and Astronautics;Shanghai Institute of Spaceflight Control Technology;
..............page:455-460
General forward kinematic algorism for three-chain parallel manipulator
Zhou Wanyong;Chen Wuyi;Liu Huadong;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;Beijing Aeronautical Manufacturing Technology Research Institute;
Zhou Wanyong;Chen Wuyi;Liu Huadong;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;Beijing Aeronautical Manufacturing Technology Research Institute;
..............page:461-466
Fighter maneuver control method of radar range tracking interrupt
Li Fei;Yu Lixin;Wang Long;Sui Yonghua;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
Li Fei;Yu Lixin;Wang Long;Sui Yonghua;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
..............page:467-472
Mass estimation method and its application for horizontal takeoff horizontal landing two stage to orbit system
Jiang Yazhong;Jiang Chongwen;Gao Zhenxun;Lee Chunhian;National Laboratory for Computational Fluid Dynamics;Beijing University of Aeronautics and Astronautics;
Jiang Yazhong;Jiang Chongwen;Gao Zhenxun;Lee Chunhian;National Laboratory for Computational Fluid Dynamics;Beijing University of Aeronautics and Astronautics;
..............page:473-478
Attitude dynamics and control of spacecraft with fluidic ring actuator based on the refined model
Guan Hong;Xu Shijie;School of Astronautics;Beijing University of Aeronautics and Astronautics;
Guan Hong;Xu Shijie;School of Astronautics;Beijing University of Aeronautics and Astronautics;
..............page:479-485
Nonlinear leakage model of rotary vane actuator
Wang Zeng;Jiao Zongxia;Wang Chengwen;Shang Yaoxing;School of Automation Science and Electrical Engineering;Beijing University of Aeronautics and Astronautics;
Wang Zeng;Jiao Zongxia;Wang Chengwen;Shang Yaoxing;School of Automation Science and Electrical Engineering;Beijing University of Aeronautics and Astronautics;
..............page:486-493
Spacecraft attitude estimation based on attitude-weighted kernel regression
Zhang Haopeng;Jiang Zhiguo;School of Astronautics;Beijing University of Aeronautics and Astronautics;
Zhang Haopeng;Jiang Zhiguo;School of Astronautics;Beijing University of Aeronautics and Astronautics;
..............page:494-499
Stiffness characteristics distribution of 3PRS /UPS parallel manipulator with actuation redundancy
Guo Jiangzhen;Wang Dan;Fan Rui;Chen Wuyi;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;
Guo Jiangzhen;Wang Dan;Fan Rui;Chen Wuyi;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;
..............page:500-506
Tipping calibration method for K-band hyperspectral microwave radiometer
Xie Yan;Chen Jingxiong;Miao Jungang;School of Electronic and Information Engineering;Beijing University of Aeronautics and Astronautics;
Xie Yan;Chen Jingxiong;Miao Jungang;School of Electronic and Information Engineering;Beijing University of Aeronautics and Astronautics;
..............page:507-511
Robust optimization of coupled structural-acoustic systems based on sensitivity analysis
Wang Chong;Qiu Zhiping;Wang Xiaojun;Wu Di;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;Research and Development Center;China Academy of Launch Vehicle Technology;
Wang Chong;Qiu Zhiping;Wang Xiaojun;Wu Di;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;Research and Development Center;China Academy of Launch Vehicle Technology;
..............page:512-516
State space theory and NR-LMS algorithm based method for structural dynamics parameter identification
Wang Yunfeng;Cheng Wei;Chen Jiangpan;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
Wang Yunfeng;Cheng Wei;Chen Jiangpan;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
..............page:517-522
Precise configuration of mixed message sets’ transmission mode in network partition
Tu Xiaojie;He Feng;Wu Qing;Xiong Huagang;School of Electronic and Information Engineering;Beijing University of Aeronautics and Astronautics;
Tu Xiaojie;He Feng;Wu Qing;Xiong Huagang;School of Electronic and Information Engineering;Beijing University of Aeronautics and Astronautics;
..............page:523-528
Hexahedral mesh generation method for geometric features
Chen Ruizhi;Xi Ping;Wang Shuai;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;
Chen Ruizhi;Xi Ping;Wang Shuai;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;
..............page:529-535
Method optimization of optimum measurement point selection in experiential modal analysis
Rong Shuanglong;Li Chuanri;Xu Fei;Ma Tian;School of Reliability and System Engineering;Beijing University of Aeronautics and Astronautics;
Rong Shuanglong;Li Chuanri;Xu Fei;Ma Tian;School of Reliability and System Engineering;Beijing University of Aeronautics and Astronautics;
..............page:536-543
Adaptive recovery algorithm for compressive sensing based on Fourier basis
Lü Fangxu;Zhang Jincheng;Wang Quan;Wang Yu;Air and Missile Defense College;Air Force Engineering University;
Lü Fangxu;Zhang Jincheng;Wang Quan;Wang Yu;Air and Missile Defense College;Air Force Engineering University;
..............page:544-550
Oblique flying wing supersonic airliner aerodynamic configuration parameters selection method
Hu Shuyao;Jiang Chongwen;Gao Zhenxun;Lee Chunhian;National Laboratory for Computational Fluid Dynamics;Beijing University of Aeronautics and Astronautics;
Hu Shuyao;Jiang Chongwen;Gao Zhenxun;Lee Chunhian;National Laboratory for Computational Fluid Dynamics;Beijing University of Aeronautics and Astronautics;
..............page:551-557
Camera calibration from geometric feature of spheres
Zhao Yuntao;Sun Junhua;Chen Xu;Gong Zheng;Precision Opto-mechatronics Technology Key-laboratory of Education Ministry;Beijing University of Aeronautics and Astronautics;
Zhao Yuntao;Sun Junhua;Chen Xu;Gong Zheng;Precision Opto-mechatronics Technology Key-laboratory of Education Ministry;Beijing University of Aeronautics and Astronautics;
..............page:558-563
Anti-coking performance of nozzle materials’ surface chemical modification
Li Fan;Zhu Yuelin;Huang Yanfei;Liu Yajie;School of Materials Science and Engineering;Beijing University of Aeronautics and Astronautics;National Key Laboratory for Remanufacturing;Academy of Armored Forces Engineering;
Li Fan;Zhu Yuelin;Huang Yanfei;Liu Yajie;School of Materials Science and Engineering;Beijing University of Aeronautics and Astronautics;National Key Laboratory for Remanufacturing;Academy of Armored Forces Engineering;
..............page:564-568
Probabilistic flutter analysis with uncertainties in structural stiffness
Tang Jian;Wu Zhigang;Yang Chao;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
Tang Jian;Wu Zhigang;Yang Chao;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
..............page:569-574
Calculation and selection of sequentially truncated test scheme
Yu Chuang;Wang Xiaohong;Li Qiuxi;School of Reliability and Systems Engineering;Beijing University of Aeronautics and Astronautics;
Yu Chuang;Wang Xiaohong;Li Qiuxi;School of Reliability and Systems Engineering;Beijing University of Aeronautics and Astronautics;
..............page:575-578
..............page:579