Aerospace Control 1993 Vol. Issue 2

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航天控制
Aerospace Control

Year 1993

Issue 2

Application of the Likelihood Interval Estimation in weapon Accuracy Analysis (似然区间估计在武器精度分析中的应用)

Jin Hong

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

Three Axes Attitude Stabilization of Geostationary Satellite during Apogec orbit Maneuvering (地球同步卫星远地点变轨期间的三轴姿态稳定)

Zhou Wenzhong Beijing Institute of Control Engineering

.................. page:7-15+6

The Effect of Attitude Angle Coupling on the Stability of 3-Axes Gyro Plateform (三轴陀螺平台的姿态耦合稳定性)

Wang Dezhao Beijing Institute of Control Engineering

.................. page:16-24

Method of Measurement in the Phase of Final Approaching for Rendezvous and Docking in Spce (交会对接最后逼近阶段的CCD相机测量方案)

Lin Laixing Li can Beijing Institute of Control Engineering

.................. page:25-33+84

Control Method of the Square Solar Sail with the Solar Rudders (用太阳舵控制大型挠性体太空帆的控制方法)

Luo Qingxian, Shentu Xinlin, Lu Guoxing Shanghai Auomatic Control Instrument Design Institute

.................. page:34-42+24

The Design and Simulation of Intelligent Controller for Spacecraft Orbil Control System (航天器轨道控制系统的智能设计方法与仿真)

Xu Xiaohao Liu Shuxiang Nanjing Aeronautical Institude, Department of Automatic Control

.................. page:43-49

A Mathod for Improving the Reliability of Autopilots (提高自动驾驶仪可靠性的一个途径)

Qiu Ganxing No. 803 Research Institute, Shanghai Space Bureau

.................. page:50-53

The Input and Output of General Digital Computers In Real Simulations (通用数字机在实时仿真中的输入输出)

Li Lei Beijing Aerospace Automatic Control Institude

.................. page:54-57+49

The Influence of computing frametime in HIL Simulatien (计算机帧时间对半实物仿真的影响)

Zou Wenjun Shanghai Electrical and Mechanical Sysem Engineering Research Institute

.................. page:58-62

A Digital Simulator Based on the Transputer (以Transputer为基础的数字仿真器)

Tong Yongqiang Beijing Aerospace Automatic Control Institude

.................. page:63-68

The Olympus Mission Recoveny (奥林普斯(Olympus)卫星的起死回生)

Zhang Shunying Beijing Institite of Control Engineering

.................. page:69-72+68

Evolution of The Peacekeeper Inertial Guidance Components and System Designs (“和平保卫者”导弹惯性制导器件和系统设计的进展)

Sun Mei Wang Yongping Beijing Aerospace Automatic Control Institute

.................. page:73-80+84

fen jin hao hang tian fei ji jin xing tian wen wu li xue shi yan (“奋进”号航天飞机进行天文物理学实验)

ZHAN Shengneng

.................. page:81-82

fen jin hao yu hang yuan bu shu tdrs hou jin xing shi yan (“奋进”号宇航员部署TDRS后进行实验)

ZHAN Shengneng

.................. page:82-83

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