Journal of Astronautics 2000 Issue z1 "ran shao liu dong he re jie gou " guo jia ji zhong dian shi yan shi

"ran shao liu dong he re jie gou " guo jia ji zhong dian shi yan shi

..............page:106

wei bo deng li zi tui li qi (mpt) yan jiu qu de chu bu cheng guo

..............page:83

hang tian xi tong gong cheng yu zi dong hua ji shu yan jiu suo

..............page:47

yi zhong xin xing de si fu xi tong -- bian jie gou xie bo chuan dong dian dong si fu xi tong

..............page:37

xi bei gong ye da xue gps yan jiu zhong xin

..............page:6

STRUTJET ENGINE--A NEW AEROSPACE POWER FOR THE 21st CENTURY
he guo qiang ; liu pei jin ; wang guo hui ; huang sheng hong

..............page:111-115

THE CONTROL OF BALLISTIC WARHEAD WITH VARIABLE CENTROID
zhou feng zuo ; cui li ming ; zhou jun

..............page:107-110

A FEATURE RECOGNIZING METHOD IN IMAGE MATCHING GUIDENCE
liu zuo ; zhu su peng

..............page:102-106

A STUDY OF OPTIMIZATION DESIGN FOR CONTAINERLESS PROCESSING BY ACOUSTIC LEVITATION
jie wen jun ; wei bing bo

..............page:94-101

THE NUMERICAL SIMULATION OF ELECTROMAGNETIC FIELDS WITHIN THE RESONANT CAVITY OF MICROWAVE ELECTROTHERMAL THRUSTER
yang zuo ; he hong qing ; mao gen wang ; wan wei

..............page:89-93

EXPERIMENTAL OBSERVATION ON STARTUP AND STEADY WORKINGPROCESS OF THE MICROWAVE ELECTROTHERMAL THRUSTER
mao gen wang ; han xian wei ; yang zuo ; huang xiao zuo ; he hong qing

..............page:84-88

NUMERICAL ANALYSIS OF GRAIN LARGE DEFORMATION FOR SOLID ROCKET MOTOR
qiang hong fu ; wang liang ; yu mao hong

..............page:77-83

THE EXPERT SYSTEM FOR INTEGRATED OPTIMIZATION DESIGN OF DSRR AND ITS MISSILE
he hong qing ; huang sheng hong

..............page:70-76

STUDY OF A GPS/DMU INTEGRATEN SYSTEM WITH LOW-COST
yue xiao kui ; yuan jian ping ; zheng zuo

..............page:66-69

STUDY OF ALGORITHMS OF SPACECRAFT ATTITUDE ESTIMATION USING GPS
luo jian jun ; yuan jian ping ; sun cheng qi

..............page:62-65

SATELLITE CONSTELLATION DESIGN FOR APPLICATION
li wen hua ; yuan jian ping ; zhao yu shan ; wang dang xiao

..............page:58-61

MODELING AND ANALYSIS FOR KILL PROBABILITY OF SINGLE AIR-TO-AIR MISSILE IN OMNIDIRECTIONAL ATTACK
gu liang xian ; wen bing heng

..............page:52-57

STUDY OF NONLINEAR H∞ ROBUST GUIDANCE LAW
li xin guo ; chen shi zuo

..............page:48-51

3D TEXTURE MODEL AND IMAGE SIMULATION
zhou zhen huan ; li yan jun ; zhang ke

..............page:43-47

APPLICATION OF AIRBORNE DIGITAL MAP TO LOW ALTITUDE PENETRATION
fang qun ; wang yan li

..............page:38-42

THERMODYNAMIC CALCULATION OF DEFICIENT OXYGEN SOLID PROPELLANT PRIMARY COMBUSTION
mao cheng li ; li zuo zuo

..............page:32-37

EXPERIMENTAL RESEARCH ON THE ATOMIZATION PERFORMANCE OF NEW-TYPE GAS/LIQUID COAXIAL SWIRLING NOZZLE
li jin xian ; xu min ; chen bu xue ; zhang meng zheng ; zhang ze ping ; li zuo

..............page:28-31

INFLUENCE OF THE BOUNDARY LAYER ON SUPERSONIC FLOWFIELD WITH SECONDARY INJECTION
sun de chuan ; cai ti min

..............page:23-27

NUMERICAL ANALYSIS OF SYNTHETIC FLOW FIELD BETWEEN ADJACENT MICROJETS
he gao rang ; wang liang ; zhang en zhao

..............page:18-22

NUMERICAL SIMULATION OF COVERAGE PERFORMANCE FOR SATELLITE CONSTELLATION
xu min ; cheng feng zhou ; chen shi zuo

..............page:11-17

CONFIGURATION AND ANALYSIS OF TWIN-STATION-BASED MICRO-SATELLITE NETWORKS
yuan jian ping ; fang qun ; wei juan

..............page:7-10

VIRTUAL PROTOTYPING TECHNOLOGY FOR FLIGHT VEHICLE DESIGN AND TEST
tang shuo ; chen shi zuo ; zhao jian wei

..............page:1-6