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Aerospace Control
1006-3242
1993 Issue 3
Rendezvous Between Two Spacecrafts With Coplanar Elliptic Orbits Using The Horizontal Impulse
Chen Ying;Wang Xudong;He Min Beijing Institute of Control Engineering
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page:1-12
Optimal Control Law Design for Safe Rendezvous and Docking of Between Two Spacecrafts
Jing Wuxing;Yan Di;Wu Yaohua Harbin Institute of Technology
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page:13-19
A Hierarchical Method To Solve Dynamic Differential Equation
Dong YunFeng Beijing University of Aeronautics and Astronautics
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page:20-24
Inertial Attitude Sensor Unit Consisted of Four Rate Integrating Gyros
Wu Guangyu Beijing Institute of Control Engineering
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page:25-28+12
Establishment of Practical Error Model for Separating Instrument Error of Guidance System
Zhao Min Beijing Aerospace System Engineering Institute
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page:29-35
Initial Measurements of Drifts of Gyroscope for Strapdown Inertial Systems
Song Xubin Beijing Institute of Control Devices
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page:36-43
Research on Vehicle-Board Sigral Processing and Guidance Computer for an Antiradiation Missile
Liu Yuhua et al Harbin Institute of Technology et al
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page:44-49
Satellite Simulation Center and Its Simulation System
Lin Laixing Beijing Institute of Control Engineering
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page:50-57
Application of YH-F1 Simulation Computer System in the Hardware-in-the-Loop Simulation of Launch Vehicle Control Systems
Xu GenBao Beijing Aerospace Automatic Control Institute
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page:58-66+49
A New Tool for Checking Simulation Model
Li Jinyu Beijing Aerospace Automatic Control Institude
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page:67-70
Research on The Software Packge for Supporting Digital Simulation
Geng Xiumei Bejing Aerospace Antomatie Control Institude
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page:71-75+70
mei guo yu hang ji gou jian jie
hu ying hong ;
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page:76-78
hang tian kong zhi ji shu de xian zhuang he wei lai xue shu jiao liu hui zuo hang tian kong zhi chuang kan shi zhou nian ji nian da hui hui yi jian xun
feng hui sheng ;
..............
page:79
di san jie hang tian kong zhi bian ji wei yuan hui di er ci hui yi jian bao
feng hui sheng ;
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page:80-43
hang tian kong zhi xuan ti da gang
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page:81