1006-3242
2001 Issue 1
The Reliability Model of Antiaircraft Missile System
zhang qing bo ; li wei min
zhang qing bo ; li wei min
..............page:75-81
..............page:71-74
General Simulation Frame about Controlled Spacecraft
zheng wei ; tang guo jian ; huang zuo gui
zheng wei ; tang guo jian ; huang zuo gui
..............page:67-70,74
..............page:59-66
..............page:55-58,66
..............page:48-54
The Analysis on Dynamical Stability of Winged Missile
wen yi min ; xu duo sheng
wen yi min ; xu duo sheng
..............page:41-47
Design of Strong Coupling System Controller
cui li ming ; zhou jun
cui li ming ; zhou jun
..............page:37-40
..............page:31-36,54
..............page:23-30
Normal Mode Attitude Determination Algorithm of a Sun Synchronous Satellite
liao zuo ; zhou jun ; zhou feng zuo
liao zuo ; zhou jun ; zhou feng zuo
..............page:17-22
Accuracy Analysis on the Method of Autonomous Position Determination Using Star Sensor
yang bo ; wu xiao jie ; fang jian cheng
yang bo ; wu xiao jie ; fang jian cheng
..............page:12-16
..............page:6-11
Composite Adaptive Control for Space Robot in Task Space
wang jing ; liu liang dong
wang jing ; liu liang dong
..............page:1-5