1006-3242
2006 Issue 5
..............page:封4
Comment on Design Methods for Modern Missile Autopilots
Liu Zhiping;Zhou Fengqi;Zhou Jun
Liu Zhiping;Zhou Fengqi;Zhou Jun
..............page:91-96
Realization of Autonomous Flight Control System of Mini-unmaned Aerial Vehicles
Chen Tianhua;Guo Peiyuan
Chen Tianhua;Guo Peiyuan
..............page:86-90
Random Weighting Center Fusion Estimation of Prior Distribution of SIMU Successive Test Data
Xu Junhui;Xu Donghui;Qian Peixian
Xu Junhui;Xu Donghui;Qian Peixian
..............page:82-85
Dynamic Modeling and Compensation on Thrust Measurement System of Attitude Control Rocket Motor
Ouyang Huabing;Xu Wengan
Ouyang Huabing;Xu Wengan
..............page:78-81
Design and Application of Aerospace Flight Mission Control Analysis System
Zheng Aiwu;Sun Jun;Liu Yong
Zheng Aiwu;Sun Jun;Liu Yong
..............page:72-77
Evaluation of Test Valid Period of Inertial Measurement System
Dong Yanqin;Wang Yusen;An Weilian
Dong Yanqin;Wang Yusen;An Weilian
..............page:68-71
A Bus-structure Flight Control System Based on DSP
Han Jianbin;Zhu Jihong;Zhang Heng;Sun Haisong;Zeng Shuo
Han Jianbin;Zhu Jihong;Zhang Heng;Sun Haisong;Zeng Shuo
..............page:63-67
Practices of Software Project Estimation and Measurement
Wei Wei;Shi Zhu;Zou Jun
Wei Wei;Shi Zhu;Zou Jun
..............page:58-62
Collision Detection in Visualization of Fuse and Warhead Coordination
Kong Weidong;Zhao Wenjie
Kong Weidong;Zhao Wenjie
..............page:53-57,77
Construction and Application of Digital Simulation Test Environment for Flight Control Software
Qian Jie
Qian Jie
..............page:49-52
The Application and Implemention of the Recursive Prediction Error Method Used in Identification of Servo System in Time Domain
Fang Lijun;Qu Shengli;Qian Bo;Han Jiang
Fang Lijun;Qu Shengli;Qian Bo;Han Jiang
..............page:46-48,67
Relative Orbit Design of a Chaser Tracking a Non-cooperative Target in Space
Che Rucai;Zhang Honghua
Che Rucai;Zhang Honghua
..............page:40-45
Some Key Technical Problems in the Design of Optical Sensor Used in RVD
Xie Yongchun;Zhang Hao;Shi Lei;Sun Chengqi
Xie Yongchun;Zhang Hao;Shi Lei;Sun Chengqi
..............page:35-39,45
Soft Landing Optimal Terminal Guidance Strategy of Lunar Probe
Shan Yongzheng;Duan Guangren;Liu Hongliang
Shan Yongzheng;Duan Guangren;Liu Hongliang
..............page:31-34
Key Techniques for the Guidance Navigation and Control System of Reusable Launch Vehicles During Reentry Phase
Zhang Qingzhen;Ren Zhang
Zhang Qingzhen;Ren Zhang
..............page:27-30
Study on Initial Alignment Method of SIMU Using Launch Vehicle Erection Movement
Wang Haiqing;Qian Weide;Cheng Ruineng;Yan Weigang
Wang Haiqing;Qian Weide;Cheng Ruineng;Yan Weigang
..............page:23-26
Blended Logic and Control System Design for an Interception Missile with Lateral Thrust and Aerodynamic Combination
Wang Yuhang;Yao Yu;Ma Kemao
Wang Yuhang;Yao Yu;Ma Kemao
..............page:18-22
A Method of Integrated GPS/INS System In-flight Alignment
Tan Hongli;Huang Xinsheng
Tan Hongli;Huang Xinsheng
..............page:14-17,34
1773 Fiber-optic Data Bus Technique and Application
Jiang Dezhong;Song Zhengyu;Zhou Dexiang
Jiang Dezhong;Song Zhengyu;Zhou Dexiang
..............page:10-13,22
Vortex Structure Recognition Using Fuzzy Neural Network
Yang Zhaohua;Fang Jiancheng;Wu Lin
Yang Zhaohua;Fang Jiancheng;Wu Lin
..............page:4-9
..............page:3