1000-1328
2002 Issue 2
..............page:92
Robust dynamic inversion control for BTT missile
zhang you an ; hu yun an ; su shen bang
zhang you an ; hu yun an ; su shen bang
..............page:89-91
Numerical simulation of slosh of the propellant fuel during the period of shut-down of the rocket
bao guang wei ; wang zhen qiang ; zhang tian xiang ; chen jian
bao guang wei ; wang zhen qiang ; zhang tian xiang ; chen jian
..............page:84-88
A discussion on satellite-network autonomous orbit determination
zuo ye ; zhou bo zhao ; ren zuo
zuo ye ; zhou bo zhao ; ren zuo
..............page:80-83
The application of wavelet transform in remote signal detection
yang zuo yuan ; jiang ; deng yong ; guo lei
yang zuo yuan ; jiang ; deng yong ; guo lei
..............page:77-79
Optimization of tactical missile effectiveness in absence of air defenses to group targets based on genetic algorithm
wang min le ; gao xiao guang
wang min le ; gao xiao guang
..............page:73-76
Vibration analysis and experiment investigation for a typical rigid-flexible coupling system
yang hui ; hong jia zhen ; yu zheng yue
yang hui ; hong jia zhen ; yu zheng yue
..............page:67-72
An investigation into the problem of evaluating combat effectiveness for missile weapon systems
zhang ke ; liu yong cai ; guan shi yi
zhang ke ; liu yong cai ; guan shi yi
..............page:58-66
Observability analysis of SINS' error states
wu mei ping ; hu xiao ping
wu mei ping ; hu xiao ping
..............page:54-57,76
The error transfer's analysis of measure criterion on a rocket-flight appraisal simulator
gao bo ; huang xi zuo ; che zhu ming ; li wen xing
gao bo ; huang xi zuo ; che zhu ming ; li wen xing
..............page:50-53
Application of a similar quadratic optimization control method in the autonomous docking control
liu zhong han ; wu hong zuo
liu zhong han ; wu hong zuo
..............page:44-49
Research of liquid rocket engine fault diagnosis method based on model knowledge
liu hong gang ; wu jian jun ; chen qi zhi
liu hong gang ; wu jian jun ; chen qi zhi
..............page:41-43,49
Effect of base contour on aerospike nozzle performance
dai wu ye ; liu yu ; zhang zheng ke
dai wu ye ; liu yu ; zhang zheng ke
..............page:34-40
Optimized performance calculation in multi-parameter for aerospike nozzle
zuo li zi ; liu yu ; wang yi bai
zuo li zi ; liu yu ; wang yi bai
..............page:28-33
Study on rigid-flexible coupling dynamics of space-based manipulator
liu jin yang ; hong jia zhen
liu jin yang ; hong jia zhen
..............page:23-27,33
The analysis and prediction of fluctuating pressure on the sphere-biconic reentry vehicles
zhang zhi cheng ; chen wei fang ; shi yu zhong ; wang quan li ; wu qi fen
zhang zhi cheng ; chen wei fang ; shi yu zhong ; wang quan li ; wu qi fen
..............page:19-22
Thermal radiation calculation in heat receiver cavity of SDPS
hou xin bin ; yuan xiu gan
hou xin bin ; yuan xiu gan
..............page:15-18
Heat and mass transfer analysis of a metal hydride heat sink for EVA spacesuit
yu min xian ; lin gui ping
yu min xian ; lin gui ping
..............page:11-14
Thermal analysis for folded solar array of spacecraft on orbit (Ⅱ)--calculation result and analysis
cheng hui er ; yang wei hua ; shi jin miao ; fang guo long
cheng hui er ; yang wei hua ; shi jin miao ; fang guo long
..............page:6-10
An integrated heat pump-ice thermal storage scheme for thermal control system of spacecraft
li ming hai ; ren jian xun ; liang xin gang ; guo zeng yuan
li ming hai ; ren jian xun ; liang xin gang ; guo zeng yuan
..............page:1-5