Application of technology readiness assessment method in flight test
ZHU Jiang-hui;SUN Yong-jun;ZHOU Zhan-ting;Department of Science and Technology;Chinese Flight Test Establishment;

..............page:193-195+204

Research of STOVL aircraft flying qualities
CHEN Kun;SHI Zhi-wei;CHEN Yong-liang;College of Aerospace Engineering;NUAA;

..............page:196-200

Lateral and directional flight quality assessment based on ground flight test results
HOU Shi-fang;XU Jian;YANG Bo-wen;Research and Development Center;AVIC Aircraft Co.;Ltd;

..............page:201-204

Design of UAVs formation controller based on ADRC control technology
LI Yi-bo;HU Yang;CHEN Wei;WANG Yi;School of Automation;Shenyang Aerospace University;Technology Center;AVIC Chengdu Aircraft Industrial CO.;Ltd;

..............page:205-208

Modelling and simulation of the double pendulum of the actively stabilized drogue and hose
SHI Chao;XUE Jian-ping;DONG Xin-min;WANG Jian;CHEN Yong;Aeronautics and Astronautics Engineering College;AFEU;

..............page:209-212+217

Investigation on the methods for estimating aerodynamic characteristics for slender body at high angle of attack
ZHU Ying;LIU Zhen;TANG Rui-qing;BU Chen;DONG Long-lei;School of Aerospace;Xi’an Jiaotong University;

..............page:213-217

Ultra-low altitude airdrop controller design based on adaptive parameter estimation backstepping
CHANG Yun-gang;SUN Xiu-xia;DONG Wen-han;LI Da-dong;LIU Ri;Aeronautics and Astronautics Engineering College;AFEU;95039 Unit of the PLA;

..............page:218-221+231

Multi-mode switching control study for near space vehicle
GU Chen-feng;JIANG Ju;ZHEN Zi-yang;WU Yu-shan;College of Automation;NUAA;

..............page:222-225

Terminal guidance of maneuvering vehicle with multiple constraints based on backstepping design
HONG Gong-ming;CHEN Wan-chun;School of Astronautics;BUAA;

..............page:226-231

Multi-constrained guidance strategy with ignition window restriction for initial descending phase of ALCM
HU Jin-chuan;CHEN Wan-chun;School of Astronautics;BUAA;

..............page:232-237+242

Design of double line-of-sight angle proportion-differential active defense guidance law
WANG Zhe;WANG Xiao-ping;LIU Zhe;DI Fang-xu;CHENG Jian-feng;Aeronautics and Astronautics Engineering College;AFEU;Theory Training Department;Airforce Xi’an Flying Academy;

..............page:238-242

Iterative guidance method of changeable launching plane flight missile
WANG Ji-ping;WEI Shi-hui;XIAO Long-xu;LIN Hong-bin;GE Pei-hong;The Second Artillery Equipment Institute;96271 Unit of the PLA;

..............page:243-247+252

Univariate fusion robust predictive control for hypersonic vehicle
FU Liang;MA Ya-lei;CAI Yuan-li;Institute of Control Engineering;Xi’an Jiaotong University;

..............page:248-252

Visual angle research for midcourse and terminal guidance hand-over of near space hypersonic vehicles
ZHAO Jie;WANG Jun;ZHANG Da-yuan;XIAO Zeng-bo;LI Qing-liang;Air and Missile Defense College;Air Force Engineering University;93507 Unit of the PLA;95100 Unit of the PLA;

..............page:253-256+260

Real time atmosphere density estimation of super low altitude with variable mechanical energy
WEN Sheng-lin;YAN Ye;College of Aerospace Science and Engineering;NUDT;

..............page:257-260

A high safety method for flutter boundary prediction
ZHONG Hua-shou;ZHANG Wei-wei;XIAO Hua;YE Zheng-yin;School of Aeronautics;NWPU;AVIC Aeronautical Science and Technology Key Laboratory of Flight Simulation;CFTE;

..............page:261-264+268

Simulator aerodynamic model calibration method based on the flight test
LIU Qing;LIU Ya-hui;ZHANG Wen-shuai;AVIC Aeronautical Science and Technology Key Laboratory of Flight Simulation;CFTE;National Key Laboratory of Civil Aircraft Flight Simulation;Shanghai Aircraft Design and Research Institute;

..............page:265-268

Research on civil aircraft near-ground flight modeling and accident recurrence during takeoff and landing
YUAN Xin;GAO Zhen-xing;Laboratory Engineering Technology Center for Flight Simulation and Advanced Training;NUAA;National Key Laboratory of Civil Aircraft Simulation Flight;

..............page:269-273+279

Autonomous flight controller design of UAV
GAO Jiu-zhou;JIA Hong-guang;Changchun Institute of Optics;Fine Mechanics and Physics;Chinese Academy of Science;Univercity of Chinese Academy of Science;

..............page:274-279

Research on attitude adjust method of stratospheric airship based-on liquid ballast
HE Xiao-hui;Center for Balloon Aerostat Research;Academy of Optoelectronics;Chinese Academy of Science;

..............page:280-283

Research on model and algorithm of diversion under flight conflict
WANG Li-li;ZHOU Juan;Tianjin Key Lab of Operation Programming and Safety Technology of Air Traffic Management;CAUC;

..............page:284-288

fei xing li xue zheng gao jian ze

..............page:290