The Simulation of the Satellite's Spin Based on MATLAB/Simulink
wang jing ; liao zuo ; peng bo yong
wang jing ; liao zuo ; peng bo yong
..............page:78-80
Study on Dynamic Properties of Missile Model Under Water
wang cong ; zhang jia zhong ; dong cai feng ; dai shu jing
wang cong ; zhang jia zhong ; dong cai feng ; dai shu jing
..............page:74-77
Study of the Formulation of Pyrotechnic Base-bleeding Agentfor Base Drag Reduction and Range-extending of Projectiles
hao jian chun
hao jian chun
..............page:71-73
The Research on Flying Simulated Drone of Skimming Sea Missile
wang bao cheng ; sun de bao
wang bao cheng ; sun de bao
..............page:67-70
Method Study of The Normal Force Engineering Calculation of Missile with Non-circular Shape Cross Sections
li xiao bin ; liu jun ; guo zheng
li xiao bin ; liu jun ; guo zheng
..............page:63-66
The Method to Obtain the Angle Error Signals of Coordinators Under the Function of MMW Frequency Step Target Identification
yang jun ; ou yang xiao li
yang jun ; ou yang xiao li
..............page:21-25
An Initial Guidance of Long- and Medium- Range Ground to Air Missiles
ding jing tao ; zhou feng zuo ; zhou jun
ding jing tao ; zhou feng zuo ; zhou jun
..............page:26-28,32
..............page:29-32
Application of Variable Structure Control in Designing of the Controller of a Guided Bomb
meng xiu yun ; zhang yong
meng xiu yun ; zhang yong
..............page:33-35,39
The Way of Improving the Anti-personnel Performance of the Anti-armor and Anti-personnel Dual Purpose Grenade
zhao yu qing
zhao yu qing
..............page:36-39
Experimental Research on Shot-proof Properties to High-speed Fragment of Heterogeneous Composite Structural Target
luo jun ; tang rui feng ; wang tie fu ; yi wen jun
luo jun ; tang rui feng ; wang tie fu ; yi wen jun
..............page:40-43
Study on Isothermal Forming Technology for Complex Empennage
feng zai xin ; zhang zhi min ; fang min
feng zai xin ; zhang zhi min ; fang min
..............page:44-45,48
Evaluation Method of Multiple Launcher Rocket System Based on Uniform Approximation
ma yan qin ; ma da wei
ma yan qin ; ma da wei
..............page:46-48
Analysis of Shock Wave Test Data in Launching Exhaust Field with Complicated Noise
zhang fu xiang ; xu qiang
zhang fu xiang ; xu qiang
..............page:49-52
Genetic Algorithms and It's Use in Solid Rocket Optimizing Design
jie hong yu ; zhang wei hua ; li xiao bin ; wang min yi
jie hong yu ; zhang wei hua ; li xiao bin ; wang min yi
..............page:53-55
A Method to Study Fire Precision of Projectile Effected by Random Factors
wu hong ; zhao you shou
wu hong ; zhao you shou
..............page:56-59
Research of Wind Compensation of Software Fire Table for Rocket
liu wen ; zhang wei hua ; zhou zuo jing
liu wen ; zhang wei hua ; zhou zuo jing
..............page:60-62
..............page:1-4
Decoupling Control of Missile by Output Feedback Eigenstructure Assignment
li fan ; zhou feng zuo ; zhou jun
li fan ; zhou feng zuo ; zhou jun
..............page:5-8
Optimum Design Method of General Parameters of HVM
cong zhi zuo ; wen zhong hui
cong zhi zuo ; wen zhong hui
..............page:9-13
The Design of Gyro Control System of Tracker Coordinator
shen ji ; zhang wei ; qi zai kang
shen ji ; zhang wei ; qi zai kang
..............page:14-17
Quick Evaluation Method for Hit Accuracy and Hit Accuracy Error Analysis of Missile
jin xing ; hong yan ji ; wen ming ; li jun mei ; li xiao min
jin xing ; hong yan ji ; wen ming ; li jun mei ; li xiao min
..............page:18-20,25