Flight Dynamics 2011 Issue 1 Study on aerodynamic characteristics of tactical missile with morphing wings

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Flight Dynamics
1002-0853
2011 Issue 1

Study on aerodynamic characteristics of tactical missile with morphing wings
ZHANG Gong-ping;DUAN Chao-yang;LIAO Zhi-zhong

..............page:54-58

Improved method for fast path planning
LIU Xi;ZHU Fan;CAI Man-yi;CHEN Bing

..............page:89-92

fei xing li xue zheng gao jian ze

..............page:封底

Flight test performance error analysis of the platform inertial navigation system
ZHANG Dong-rong;YE Bin;DANG Jin

..............page:74-77

Modeling and simulation of solar-powered airplane for the conceptual design
ZHAO Kai;ZHU Xiao-ping;ZHOU Zhou

..............page:13-16

Study on interacting multiple-model based fault tolerant flight control
DENG Sheng-li;LEI Hu-min;SHAO Lei;SHE Sheng-lu

..............page:34-37

Design of optimal guidance law for interception ballistic missile during the boost phase
CUI Yan-kai;LIANG Xiao-geng;WANG-Fei;HU Yan-na

..............page:59-62

Research on airport runway ultimate capacity model
MENG Xiang-wei;ZHANG Ping;LI Chun-jin

..............page:78-83

Low speed reflexed airfoil robust optimization design for flying wing configuration
LI Jun-peng;WANG He-ping;GE Wen-jie

..............page:17-20

UAV control method studied based on high-order sliding mode control
HOU Hai-ping;WEI Rui-xuan;LIU Yue;ZHOU Wei;WEI Chuan

..............page:38-41,58

Robust adaptive controller design for a hypersonic vehicle based on characteristic model
SUN Qi;ZHOU Jun;LIN Peng

..............page:46-49

Design of the relay switch guidance handover scheme for interception of the ship-air missile
ZHAO Yong-tao;HU Yun-an;LI Jing

..............page:50-53

Model predictive control approach to three-axis stabilization of gravity field satellite
JI Li;XIANG Jun-hua;LIU Kun

..............page:66-69

Mechanisms research of rain effects on airfoil aerodynamic performance
ZHANG Rui-min;CAO Yi-hua

..............page:70-73

Research on relative reachable domain of satellite trajectory generated after continuous-thrust applied
LI Xue-hua;HE Xing-suo

..............page:63-65,88

Study on longitudinal maneuverability and stability of folding wing morphing aircraft
JIN Ding;ZHANG Wei;AI Jun-qiang

..............page:5-8,12

Flight rerouting path evaluation method in air traffic
LI Xiong;XU Xiao-hao

..............page:84-88

Approach to integrated navigation and attitude determination based on GPS/magnetometer/accelerometer
LIU Kai;GUO Jian-guo;GE Zhi-lei;ZHOU Jun

..............page:93-96

Improved wind model based on the meteorological UAV flight angles
ZHOU Shu-dao;WANG Yan-jie;WANG Min;ZHU Guo-tao;CHENG Long

..............page:26-29

Full-envelop control laws design and its simulation for a helicopter\'s coordinated turning motion
XING Xiao-jun;YAN Jian-guo

..............page:42-45

Study on stability and controllability of flying wing UAV
CHENG Xue-mei

..............page:9-12

Research on longitudinal attitude control technology of tilt rotor during transition
CHEN Yong;GONG Hua-jun;WANG Biao

..............page:30-33

Performance analysis of waverider with blunt leading edge in off-design regimes
LIU Ji-min;HOU Zhi-qiang;SONG Gui-bao;WANG Yun-liang

..............page:21-25

Calculation for lift-drag characteristics based on civil airplane\'s take-off performance
WU Zhao;WANG Li-xin

..............page:1-4