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Journal of Projectiles, Rockets, Missiles and Guidance
2003 Issue 1
zhong guo you xiu bo shuo shi xue wei lun wen quan wen shu ju ku (cdmd) zong ti jie shao
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page:附2
Lyapunov Function Stabilization-Based Design of Aerodynamic Missile Block Diagonal Controller
shang an li ; gu wen jin ; guo zhen kai
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page:1-4
2003 nian guo ji tui jin ji zha yao yan huo ji shu qiu ji yan tao hui
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page:附1
Applications of Silicon Accelerometer in Terminally Guided Projectile Test
sun zhi ming
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page:91-93
Experimetal Studies of Confined High Pressure Discharges in Piccolo Capillary
wang zheng lun ; cheng jian ; li bao ming
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page:88-90
Research on Satellite Positioning System of Differential GPS
zhang zuo ; zhang liang ; lian bao wang
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page:85-87
Image Compression Based on wavelet Transform
he feng hua
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page:83-84,87
Study on Sequence-Split in Radio-Location System
chen hui ; zuo bao zhong ; yuan rui ming ; yuan qing sheng
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page:79-82
Ultraviolet Optic-Electronic Passive Warning
che shuang liang ; zhou jun ; xu ming shun ; zhang xing she ; zhu mai hua
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page:76-78,82
Ouickly Calculation Method of Lower Confidence Limit of Normal Probability with Specified Limits
jin xing ; hong yan ji ; wen ming ; li jun mei
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page:73-75
A New Boolean Calculation Method and it's Application of Reliability Analysis
jin xing ; hong yan ji ; wen ming ; li jun mei
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page:69-72
A Compact Hybrid Genetic Algorithm in Aerodynamic Optimization Design
wang xiao peng
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page:65-68
The Dynamic Characteristics Analysis of High Speed Slender Rocket
tian xiao li ; chen guo guang
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page:62-64
The Design of Work Order of the Base-Bleed-Rocket Unit By the Taguchi Method
li tie peng ; qian jian ping ; li yue jie ; zhang bing ling
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page:59-61,64
Experiment Study on a New Infantry Ammunition for Storming Fortification
li chun lin ; xie le ping
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page:57-58
A Study of Objects Seperating Move Law Under Slice Powder
feng shun shan ; jia guang hui
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page:54-56
Amplitude Frequency Characteristics of Seismic Event Caused by the Near-ground Cloud Detonation
xiong zu zuo ; lin da chao
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page:50-53
Ultrasonic Technique for the Welds in the Steel Pipes with Different Thickness
yang lu ; han zuo ; cheng yao zuo
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page:47-49,53
The Experiment and Simulation Research of Initial Alignment of the Strapdown Inertial Guidance System of Short Range Missile
qi zhan yuan ; zhang jing ; li zuo
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page:42-46
Study on Reaction capability of Ground-to-Air Missile Weapon System
liu zhu he ; wen hong wei
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page:39-41
The Identification of Fractal Scaleless Band in Calculating Correlative Dimension with G.P Algorithm
dang jian wu ; wang rui ling ; huang jian guo
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page:35-38
Command Guidance System Optimal Non-dimensional Parameter Design
sun ji wei ; liu dan ; qi zai kang
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page:31-34,38
Step Frequency and PD Work-mode Analysis of MMW Guidance Radar
chen jun ke
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page:27-30
The Model of Calculating Aerial Defence Missile Kill Zone by BP Neural Network
cao ze yang ; li wei min
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page:24-26
The Design of the Optimal Redundant Structure for the Flight-Control/Inertial Integrated System MIRA and the Research for Redundancy Management
zhang jing mei ; gao she sheng ; guo fu qiang
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page:21-23
The Variable Structure Adaptive Control and its Application to Missile Attitude Control System
xu hua long ; zhao da zuo ; chen guang jun ; wang wu yi
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page:17-20
Realization of Missile Simulator's Animation Based On OpenGVS
wu chun bo ; zhang jing
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page:13-16
A Fault-diagnosis Expert System for the Test-Firing Control Systems of Missiles Based on Neural Network Method
bi shi hua ; liu wen zuo
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page:9-12
Effect of Direction Error on Guidance Performance of Spinning Missiles
wang zong yi
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page:5-8