1006-3242
2009 Issue 5
wei xing zi zhu gu zhang zhen duan zhuan jia xi tong zhong zhi shi ku de she ji
jiang lian xiang ; li hua wang ; yang gen qing
jiang lian xiang ; li hua wang ; yang gen qing
..............page:93-97
Research on Application of Life Cycle Cost Management
li zuo ; zheng chun sheng ; sui dian ben
li zuo ; zheng chun sheng ; sui dian ben
..............page:98-101,105
huan jing yin zi de fei can shu zhi xin xian
sun zhu ling
sun zhu ling
..............page:102-105
An Overview on Development of Bank-to-Turn Technology for Tactical Missiles
ye zhen xin ; fu wei xian ; wang wan jun ; li ya hui ; wang yong zuo
ye zhen xin ; fu wei xian ; wang wan jun ; li ya hui ; wang yong zuo
..............page:106-112
Application of the Multi-objective Evolutionary Algorithm in Midcourse Correction of Spacecraft Transfer Orbit
wang meng yi ; jiang yong
wang meng yi ; jiang yong
..............page:52-57
Iteratively Updating Method of Generating Approximation Model in Multidisciplinary Design Optimization
sun zuo jie ; shen gong zuo
sun zuo jie ; shen gong zuo
..............page:58-64
Study on Relative Orbit Determination Method of Satellites Formation with Short-arc
li xiao ming ; zeng guo qiang ; yao hong
li xiao ming ; zeng guo qiang ; yao hong
..............page:48-51,57
Attitude Determination and Analysis for Engineering Application Based on Gyroscope and Magnetometer
wang xian zhong
wang xian zhong
..............page:43-47
Research on New Test-launch Control Flow Inquiry Platform
ren hui min ; liu jun yang ; wang xiao ling ; qi zhu yun ; he feng
ren hui min ; liu jun yang ; wang xiao ling ; qi zhu yun ; he feng
..............page:83-86,92
Correction Algorithms to Truncation Error in Trajectories of Carrier Rocket
chai min ; hu shao lin ; guo xiao hong
chai min ; hu shao lin ; guo xiao hong
..............page:87-92
Application Mission Modeling of Reconnaissance Satellite Based on PDDL
fan zhi liang ; wang di ; ren hai yan ; ma man hao
fan zhi liang ; wang di ; ren hai yan ; ma man hao
..............page:77-82
The USB TT&C System and Realization of Simulation
xu jian zhong ; wang zu lin ; guo xu jing ; zhao yi zuo ; tu zuo zuo
xu jian zhong ; wang zu lin ; guo xu jing ; zhao yi zuo ; tu zuo zuo
..............page:65-69
Decoder Chip ASIC Design of Remote Control Car with Study Function
wang xiao hua ; zhou song qing ; luo xiao shu ; yin yan gang
wang xiao hua ; zhou song qing ; luo xiao shu ; yin yan gang
..............page:70-76,82
Guidance Precision Modeling of Air Defense Misslie Intercepting Formation Targets
zhang shu zheng ; zhou feng zuo ; jiang de sheng
zhang shu zheng ; zhou feng zuo ; jiang de sheng
..............page:11-14,19
..............page:20-23
Analysis of Pdop Value of Position by Three Stations or by Four Stations of Ground Based Navigation
wang dan dan ; wang xiao jun ; chen xiao jun ; fu wei xian
wang dan dan ; wang xiao jun ; chen xiao jun ; fu wei xian
..............page:15-19
The Error Analysis of C-W Guidance
ma yan hong
ma yan hong
..............page:38-42,47
Integrated Orbit and Attitude Determination Algorithm for Small Satellite
xing yan jun ; zhang shi jie ; cao xi bin
xing yan jun ; zhang shi jie ; cao xi bin
..............page:31-37
Nonparametric Modeling and Filtering of Laser Gyro Random Error
he zhi kun ; wang xue mei
he zhi kun ; wang xue mei
..............page:24-27,37
..............page:28-30
Study On Nonlinear Three-dimensional Variable Structure Robust Adaptive Guidance Law
chang ying ying ; shi xiao ping
chang ying ying ; shi xiao ping
..............page:7-10
Dynamic Inversion Controller Design of UAV Based on NN
li zuo yong ; shen huai rong
li zuo yong ; shen huai rong
..............page:3-6