Aerospace Control 1997 Vol. Issue 2

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航天控制
Aerospace Control

Year 1997

Issue 2

Verification of Aerodynamic Parameters of Missile Using Flight Test Data (利用飞行试验数据校验导弹气动参数)

Qiu Ganxing

.................. page:1-5

Influence of Lever Arm Effect in Platform Inertial Navigation System of Launch Vehicle on Injection Accuracy (运载火箭平台惯导系统杆臂效应对入轨精度的影响)

Zhou Manjuan

.................. page:6-11

Constrained Variance and H_∞ Output Feedback Control for a Class of Engineering System with Measurement Noise (一类工程系统的约束方差/H_∞输出反馈控制:含测量噪声的情形)

Wang Zidong, Guo zhi

.................. page:12-16+22

Adaptive Filtering Approach for Missile Flight Test Trajectory Determination Under Multiple Station Measuring (导弹飞行试验多站测量定轨的自适应滤波方法)

Cai Hong, Zhang Jinhuai

.................. page:17-22

RQP Based Finite Thrust Apogee Orbit Transfer with Minimum Fuel (基于递推二次规划算法的燃料最优有限推力远地点变轨)

Zhao Xu, Li Guo, Li Tieshou

.................. page:23-28

Fuzzy Control of Flexible Structure Satellite on Single Axis Air Bearing Table (挠性结构卫星单轴气浮台的模糊控制)

Sun Qing, Wu Hongxin

.................. page:29-36+64

A Regional Positioning System Concept (一种区域定位系统的概念)

Yu Shaohua Sun Lianqin

.................. page:37-42

Application of Computer Network Technology in Aerospace Measurement and Control Area (计算机网络技术在航天测控领域的应用)

Han Shuwang, Zhao Yumei, Qian Ling

.................. page:43-50

Simulation Method Study of Strapdown Celestial Guidance (捷联星光制导仿真方法研究)

Xiao Chenggui

.................. page:51-57

Application Perspective of High and New Technique in System Simulation (高新技术在系统仿真中的应用前景)

Xu Gengbao, Gan Shengru

.................. page:58-64

Developing High Efficiency Stress Screening Test and Improving Missile Reliability (开展高效应力筛选试验提高导弹可靠性)

Wu Wei, Zheng Feng, Xu Jinghua

.................. page:65-69

Missile Guidance Technique Faced with New Challenge (导弹制导技术面临的新挑战)

Wang Yongping

.................. page:70-75+42

Advances in the Spacecraft Autonomous Navigation Technology (航天器自主导航技术的新进展)

Li Jie, Chen Yiqing

.................. page:76-81+11

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