Aerospace Control 1997 Issue 2 Verification of Aerodynamic Parameters of Missile Using Flight Test Data

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Aerospace Control
1006-3242
1997 Issue 2

Verification of Aerodynamic Parameters of Missile Using Flight Test Data
Qiu Ganxing

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

Influence of Lever Arm Effect in Platform Inertial Navigation System of Launch Vehicle on Injection Accuracy
Zhou Manjuan

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

Constrained Variance and H_∞ Output Feedback Control for a Class of Engineering System with Measurement Noise
Wang Zidong;Guo zhi

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

Adaptive Filtering Approach for Missile Flight Test Trajectory Determination Under Multiple Station Measuring
Cai Hong;Zhang Jinhuai

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

RQP Based Finite Thrust Apogee Orbit Transfer with Minimum Fuel
Zhao Xu;Li Guo;Li Tieshou

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

Fuzzy Control of Flexible Structure Satellite on Single Axis Air Bearing Table
Sun Qing;Wu Hongxin

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

A Regional Positioning System Concept
Yu Shaohua Sun Lianqin

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

Application of Computer Network Technology in Aerospace Measurement and Control Area
Han Shuwang;Zhao Yumei;Qian Ling

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

Simulation Method Study of Strapdown Celestial Guidance
Xiao Chenggui

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

Application Perspective of High and New Technique in System Simulation
Xu Gengbao;Gan Shengru

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

Developing High Efficiency Stress Screening Test and Improving Missile Reliability
Wu Wei;Zheng Feng;Xu Jinghua

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

Missile Guidance Technique Faced with New Challenge
Wang Yongping

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

Advances in the Spacecraft Autonomous Navigation Technology
Li Jie;Chen Yiqing

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