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Flight Dynamics
1002-0853
2001 Issue 2
mei jun xian yi wu ren ji jin xing shi dan she ji shi yan
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page:61
ji yu pc ji de xu ni xian shi fei xing xun lian xi tong yi zhu jian jin ru shi ji ying yong
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page:8
Backstepping-based variable structure control for a class of nonlinear systems and its application
hu yun an ; zhang you an ; song zhao qing ; cui ping yuan
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page:83-86
Dynamics model of large flexible liquid-filled satellite
peng dong liang ; nie run tu ; xu shi jie
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page:78-82
The application of PIB model to the orbit debris environment management
ma xiao yu ; cui ping yuan
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page:73-77
Research on adaptive filter algorithm and simulation for GPS/INS the integrated navigation
huang xiao rui ; cui ping yuan ; cui zuo tao
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page:69-72
Conversion results and error analysis of the level acceleration flight test on an aircraft
wang zhong ji ; zhou xiao fei
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page:65-68
Modeling and simulation of flight/propulsion system for low altitude penetration
liu guo gang ; shen chun lin ; xin ji ling
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page:30-33
Design of the tactical flight real-time optimal trajectory system
hu zuo ; xia jie ; gao jin yuan
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page:26-29
Study of failure detection methods in flight control systems
shen yi ; luo chang xing ; deng jian hua
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page:21-25
Robust method to design the integrated flight/ propulsion control system
peng ke mao ; zhao chao ; shen gong zuo ; wen chuan yuan
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page:12-16
The analysis of aerodynamic coupling effects in close formation
liu yong ; wu mi cui
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page:12-16
A practical method for flight quality parameter real time identification
li xiang ; li wei ji
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page:9-11
The analysis of Cobra maneuver and rebuild of some movement parameters
wang qi ; wu ju ying
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page:5-8
Study on certification performance flight test methods of civil transport aircraft
huang wen jing ; meng jian wen ; wu mi cui
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page:62-64
Research on JL8 aircraft stall and spin flight test
li xue qin ; gong xi qing ; jia xiao peng ; lv yu hu
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page:57-61
Calibration of angle of sideslip using fuzzy neural network
sun shao shan ; yang chao xu ; yang wei
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page:52-56
Verification on height laminated flight test of the fighter
chen zuo ; wu mi cui ; zhang de yuan
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page:49-51
Application of H∞ theory in design of aircraft landing control
zuo qi ; liu hui ying
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page:45-48
Study on the optimization of the LEO small satellite constellation
li wen hua ; yuan jian ping ; zhao yu shan
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page:41-44
Research on algorithm of probability of attack target in terminal
li qing zhen ; liu xin xue ; wang ming hai
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page:37-40
Gyroless spacecraft attitude and rate determination
cheng yang ; yang di ; cui zuo tao
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page:34-36
A control method based on dynamics for post-stall maneuvering
zhang shu guang ; xin yi
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page:1-4