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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
..............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
..............page:13-19
A Hierarchical Method To Solve Dynamic Differential Equation
Dong YunFeng Beijing University of Aeronautics and Astronautics
..............page:20-24
Inertial Attitude Sensor Unit Consisted of Four Rate Integrating Gyros
Wu Guangyu Beijing Institute of Control Engineering
..............page:25-28+12
Establishment of Practical Error Model for Separating Instrument Error of Guidance System
Zhao Min Beijing Aerospace System Engineering Institute
..............page:29-35
Initial Measurements of Drifts of Gyroscope for Strapdown Inertial Systems
Song Xubin Beijing Institute of Control Devices
..............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
..............page:44-49
Satellite Simulation Center and Its Simulation System
Lin Laixing Beijing Institute of Control Engineering
..............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
..............page:58-66+49
A New Tool for Checking Simulation Model
Li Jinyu Beijing Aerospace Automatic Control Institude
..............page:67-70
Research on The Software Packge for Supporting Digital Simulation
Geng Xiumei Bejing Aerospace Antomatie Control Institude
..............page:71-75+70
mei guo yu hang ji gou jian jie
hu ying hong ;
..............page:76-78