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Control Technology of Tactical Missile
1009-1300
2003 Issue 2
pu lin ( lang fang ) guang dian ji shu you xian gong si chan pin jian jie
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page:63
zui xin aiaa pian ming tong bao
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page:61-62,7
ji yu lpv bian huan de bian zeng yi dao dan zi dong jia shi yi she ji
Jeff S.Shamma;James R.Cloutier
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page:52-60
Bayesian Risk Analysis of the Dispersion Evaluation for Falling Points of Missile
liu lu hua ; zhang shi feng ; tang guo jian
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page:48-51
Design of the Test Software for a Certain Missile-Borne Computer
chen gong pu
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page:44-47
Structure Optimized Design of a kind of Actuator System
bai hui yan
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page:41-43
Analysis of the Feasibility and Reliability of Electromechanical Actuator for BTT Missile
chen zuo
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page:38-40,47
Research on the Rebalance Loop of Regulating Dynamical Parametersfor Liquid Floated Gyroscope in All Operating Temperature Range
li zheng xi
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page:32-37
Analysis of the Drift Errors with Related to g2 and Resonance-Induced for DTG
luo zuo jing ; yang jun ; song you shan
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page:26-31
A Method of Calibrating the Error Coefficient Using Navigation Datum for SINS
bai chao zuo ; li li xin
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page:20-25
Study on the Error Source of Inertial Platform during in-Alignment
liu feng ; zheng xin
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page:16-19
Adaptive Compensation Technique of the Nonlinear Errors for Gyroscope Systems
wan yan hui ; pei ting guo
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page:12-15
Method of the Accuracy Estimate for Inertial Navigation Systems during in-Flight Alignment
zhu shao ji ; su xiang rong ; guo you zhi
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page:8-11,15
Research of Helix Maneuver Control at the Terminal Trajectory of Anti-ship Missile
gu wen jin ; wang feng lian
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page:2-7