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Journals   A B C D E F G H I J K L M N O P Q R S T U V W X Y Z
Flight Dynamics
1002-0853
2013 Issue 4
Two-stage parameters identification method of unmanned helicopter based on subspace and PEM
shao ming qiang ; li guang wen ; xu heng
..............page:367-371
An alternative approach for parameter based flight loads identification using the neural networks
ma kai chao ; song bi feng ; yin zhi ping ; xie wei ; cao shan cheng
..............page:363-366,371
Flight program design for suborbital reusable launch vehicle after engine failure
wang wen hu ; li xin guo ; wang chen zuo
..............page:359-362
Robust stability analysis and its application in flight flutter test
wang dong sen ; wu zhi gang ; zhou you ming
..............page:372-375
fei xing li xue zheng gao jian ze
..............page:封4
Multi-aircraft rerouting path planning based on improved artificial potential field algorithm
wang xing long ; xu xiao hao ; feng jiang ran
..............page:381-384
Optimal deorbit research of spacecraft with variable thrust based on hp-adaptive pseudospectral method
feng bi ming ; nie wan sheng ; zheng gang
..............page:354-358,362
Fast terminal trajectory optimization for hypersonic spacecraft
yang liang ; zhou hao ; chen wan chun
..............page:341-344
Fighter plane's attacking track programming of over-the-shoulder
li hao liang ; zhang bin ; zuo xing xing
..............page:308-312
Terminal guidance law with angular constraint design for maneuvering reentry body
tao jian ; chen jie ; zhao hong chao ; li shi gai
..............page:345-348,353
The method to define the altitude of hypersonic gliding peak
lv shi ; tang shuo ; zuo xiao dong
..............page:349-353
A comparison of nonlinear dynamics inversion control law designs for a fighter aircraft
long jin wei ; pan wen jun ; wang li xin
..............page:297-300
Numerical simulation of hypersonic plasma flow fields around blunt cone model
yang peng fei ; fang yang wang ; chai dong ; gao xiang
..............page:313-316
Study on automatic flight quality evaluation with the pilot model
han xiao ning ; zhao xin kai
..............page:293-296
Simulation and application investigation for atmospheric turbulence based on rational power spectrum method
cao jiu fa ; shen hong liang ; wang tong guang
..............page:289-292,304
Research of internal air launching separation based on CFD dynamic mesh method
guo xu ; tang shuo ; liu zuo ; xu zhi
..............page:336-340
Aerial refueling modeling and close-distance maneuvering control law design for UCAV
zuo he feng ; dong xin min ; xue jian ping ; wang hai tao
..............page:326-330,340
Analysis of flight safety scale in windshear for large aircraft
wu hu zi ; geng jian zhong ; luo zhen yi ; tang chang hong
..............page:305-307,312
Visual-aided modeling and simulation of unmanned aerial vehicle autonomous aerial refueling
wang xu feng ; dong xin min ; kong xing zuo ; wang long ; cheng jian feng
..............page:331-335
Modeling of aircraft with variable mass in aerial refueling and design of disturbance compensation controller
liu jiao long ; xue jian ping ; dong xin min ; wang hai tao ; dai feng
..............page:321-325
Research on nonlinear control of automated carrier landing with the airwake rejection ability
wang qi ; wu wen hai ; hu guo cai
..............page:317-320
Study on flight control of energy extraction for small unmanned aerial vehicles
xia lu ; hu rong hua ; shang zhong yang
..............page:301-304
Research of passive integrated navigation system based on UKF for high dynamic aircraft
shao zuo ; zhu xiao ping ; zhou zhou ; zhao gang
..............page:376-380
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