1002-0853
2015 Issue 6
Prediction of wind flight safety based on radar spectral width and turbulence model
HAN Guo-xi;ZHANG Shu-guang;The First Research Institute;China Academy of Aerospace Aerodynamics;School of Transportation Science and Engineering;BUAA;
HAN Guo-xi;ZHANG Shu-guang;The First Research Institute;China Academy of Aerospace Aerodynamics;School of Transportation Science and Engineering;BUAA;
..............page:481-485
Flight simulation of large parafoil-payload systems based on multibody dynamics
CHEN Jian-ping;NING Lei-ming;ZHANG Hong-ying;TONG Ming-bo;College of Aerospace Engineering;NUAA;
CHEN Jian-ping;NING Lei-ming;ZHANG Hong-ying;TONG Ming-bo;College of Aerospace Engineering;NUAA;
..............page:486-490
Aircraft flight dynamics simulation under asymmetric ice accretion
CHEN Wei;XU Hao-jun;WANG Xiao-long;PEI Bin-bin;WANG Jian-ming;Aeronautics and Astronautics Engineering College;AFEU;
CHEN Wei;XU Hao-jun;WANG Xiao-long;PEI Bin-bin;WANG Jian-ming;Aeronautics and Astronautics Engineering College;AFEU;
..............page:491-494+499
Study on controllability and stability of flying wing and folding wing morphing aircraft
YIN Wen-qiang;AN Ran;AN Yu-jiao;Aircraft Flight Test Technology Institute;CFTE;
YIN Wen-qiang;AN Ran;AN Yu-jiao;Aircraft Flight Test Technology Institute;CFTE;
..............page:495-499
Data processing of flight tests on takeoff performance for commuter aircraft
YU Xue-mei;ZHOU Xiao-yi;GU Wei-yan;School of Architecture and Engineering;Heilongjiang University;Flight Test Department;AVIC General Aircraft Company;
YU Xue-mei;ZHOU Xiao-yi;GU Wei-yan;School of Architecture and Engineering;Heilongjiang University;Flight Test Department;AVIC General Aircraft Company;
..............page:500-504
..............page:504
Modeling and relative motion analysis of multi-body nonlinear dynamic of powered parafoil
CHEN Zi-li;ZHANG Hao;QIU Jin-gang;Department of UAV Engineering;Ordnance Engineering College;
CHEN Zi-li;ZHANG Hao;QIU Jin-gang;Department of UAV Engineering;Ordnance Engineering College;
..............page:505-509
..............page:509
Analysis of flutter and chaos of long straight wing
XIAO Yan-ping;YANG Yi-ren;LU Li;Flight Technology College;Civil Aviation Flight University of China;School of Mechanics and Engineering;Southwest Jiaotong University;
XIAO Yan-ping;YANG Yi-ren;LU Li;Flight Technology College;Civil Aviation Flight University of China;School of Mechanics and Engineering;Southwest Jiaotong University;
..............page:510-513+518
Research on robustness for gust alleviation aeroservoelastic system of elastic aircraft
LIU Fu-hu;MA Xiao-ping;Strength Department;Shanghai Aircraft Design and Research Institute;School of Aeronautics;Northewestern Polytechnical University;
LIU Fu-hu;MA Xiao-ping;Strength Department;Shanghai Aircraft Design and Research Institute;School of Aeronautics;Northewestern Polytechnical University;
..............page:514-518
Research of pilot control strategy to pursuit flight path in carrier landing
ZHAO Zhen-yu;HAN Wei;CHEN Jun-feng;Department of Airborne Vehicle Engineering;NAAU;
ZHAO Zhen-yu;HAN Wei;CHEN Jun-feng;Department of Airborne Vehicle Engineering;NAAU;
..............page:519-522
Longitudinal damping controller for UAV based on L1 adaptive control
WANG Liang-liang;LIU Xiao-xiong;MA Qing-yuan;XU Heng;College of Automation;NWPU;
WANG Liang-liang;LIU Xiao-xiong;MA Qing-yuan;XU Heng;College of Automation;NWPU;
..............page:523-526
Nonlinear control based on nonlinear gain of hypersonic vehicle
LIANG Shuai;SUN Xiu-xia;LIU Shu-guang;LIU Xi;TANG Qiang;Aeronautics and Astronautics Engineering College;AFEU;Key Laboratory of Integrated Aircraft Control;Xi’an Flight Automatic Control Research Institute;
LIANG Shuai;SUN Xiu-xia;LIU Shu-guang;LIU Xi;TANG Qiang;Aeronautics and Astronautics Engineering College;AFEU;Key Laboratory of Integrated Aircraft Control;Xi’an Flight Automatic Control Research Institute;
..............page:527-531
Cruise flight controller design for a hypersonic vehicle
ZHAO Lin-dong;TANG Sheng-jing;School of Aerospace Engineering;Beijing Institute of Technology;
ZHAO Lin-dong;TANG Sheng-jing;School of Aerospace Engineering;Beijing Institute of Technology;
..............page:532-536
Research on complex control for multi-purpose combat aircraft
ZHAN Zheng-yong;CUI Yu-wei;Department of Flight Control;AVIC Xi’an Flight Automatic Control Research Institute;
ZHAN Zheng-yong;CUI Yu-wei;Department of Flight Control;AVIC Xi’an Flight Automatic Control Research Institute;
..............page:537-541+550
Design of flight controller based on grey-prediction sliding mode control
JIAO Xin;JIANG Ju;MENG Hong-peng;College of Automation Engineering;NUAA;
JIAO Xin;JIANG Ju;MENG Hong-peng;College of Automation Engineering;NUAA;
..............page:542-546+550
An approach to data preparation of closed loop guidance based on BP neural network
XIAN Yong;LI Shao-peng;LI Zhen-hua;LIU Bing-qi;The Seventh Department;The Second Artillery Engineering University;
XIAN Yong;LI Shao-peng;LI Zhen-hua;LIU Bing-qi;The Seventh Department;The Second Artillery Engineering University;
..............page:547-550
Research on the near-earth spacecraft quantum positioning determinacy algorithm
WANG Zhi-gang;YANG Xuan;DENG Yi-fan;College of Astronautics;NWPU;National Key Laboratory of Aerospace Flight Dynamics;
WANG Zhi-gang;YANG Xuan;DENG Yi-fan;College of Astronautics;NWPU;National Key Laboratory of Aerospace Flight Dynamics;
..............page:551-554
Handling quality rating technology with system failure based on HQRM
ZHANG Hai-ni;JIA Xiao-peng;CHENG Wei-hao;Aircraft Flight Test Technology Institute;CFTE;
ZHANG Hai-ni;JIA Xiao-peng;CHENG Wei-hao;Aircraft Flight Test Technology Institute;CFTE;
..............page:555-559
zhong guo fei xing li xue yu fei xing shi yan di 31 jie xue shu jiao liu nian hui zheng wen tong zhi
..............page:559
A methodology of non-stationary degree suitable for FTPVS data processing
TAN Bo;ZHENG Hua;PEI Cheng-ming;School of Power and Energy;NWPU;
TAN Bo;ZHENG Hua;PEI Cheng-ming;School of Power and Energy;NWPU;
..............page:560-564
LPV modeling of morphing UAV based on improved function-substitution method
WU Cheng-fu;SHAO Peng-yuan;National Key Laboratory of Special Technology on UAV;NWPU;
WU Cheng-fu;SHAO Peng-yuan;National Key Laboratory of Special Technology on UAV;NWPU;
..............page:565-568+573
Researches on the helicopter flight test methods for vertical climb performance
SHEN Li;LI Liang-ming;ZHAO Jing-chao;Aircraft Flight Test Technology Institute;CFTE;
SHEN Li;LI Liang-ming;ZHAO Jing-chao;Aircraft Flight Test Technology Institute;CFTE;
..............page:569-573
..............page:574-576
..............page:578