1009-1300
2011 Issue 2
Design of the three-dimensional optimal terminal guidance law based on the active disturbance rejection and terminal sl
lv yong jia ; zhang he xin ; fan jin suo ; wu yu bin ; li zheng wen
lv yong jia ; zhang he xin ; fan jin suo ; wu yu bin ; li zheng wen
..............page:10-15
Design method of aerocraft PID controller parameter based on gain- phase margins tester method
li meng ; wang xiao yu
li meng ; wang xiao yu
..............page:16-21
..............page:45-48,62
Design and implementation for simulation platform of the UAV flight control system based on reapid prototyping technolo
wang yi zuo ; che jian guo ; hu yan lin ; zhong le
wang yi zuo ; che jian guo ; hu yan lin ; zhong le
..............page:49-56
Research on long-term repeatability of tactical missile＇ s SIMU
liu shuang ; liu yong yuan ; mo ming gang ; li hai qiang
liu shuang ; liu yong yuan ; mo ming gang ; li hai qiang
..............page:27-34
Optimal control in missile reentry stage little trajectory obliquity attack question
chai bin ; zuo zuo
chai bin ; zuo zuo
..............page:1-6
..............page:22-26
Research of controllable-rolling electric actuator system
cheng jian wei ; song xin bo ; zhang dong xu ; yao xiao xian
cheng jian wei ; song xin bo ; zhang dong xu ; yao xiao xian
..............page:35-39
Research on algorithm of fault diagnose for a certain aircraft ground power
wu yu bin ; zhang he xin ; lv yong jia
wu yu bin ; zhang he xin ; lv yong jia
..............page:57-62
Design and simulation of a target missile＇ s trajectory and flight control law
wang jun bo ; tian yuan ; song xun ; ren zhang
wang jun bo ; tian yuan ; song xun ; ren zhang
..............page:40-44
Study on self_calibration technique of four-gimbals platform inertial navigation system paraments
xu zhi gang ; zhao dong yan
xu zhi gang ; zhao dong yan
..............page:7-9
..............page:F0004-F0004