1006-3242
2006 Issue 6
..............page:84-89
The Research of Flight Control Software Reuse in Control System
Meng Xiaofeng;Ma Weihua
Meng Xiaofeng;Ma Weihua
..............page:81-83,89
..............page:77-80
The Fault Tolerance Technique and Theory Based on Evolvable Hardware
Gong Jian;Yang Mengfei
Gong Jian;Yang Mengfei
..............page:72-76,80
Fault Diagnosis for GNC Subsystem of Spacecraft Based on the Fuzzy Neural Network Techniques
Cai Biao;Wang Nanhua
Cai Biao;Wang Nanhua
..............page:67-71
Fault Diagnosis for Satellites Based on RBF Neural Network and Mahalanobis Distance
Yan Fei;Qin Shiyin
Yan Fei;Qin Shiyin
..............page:61-66
GNSS Ground-based Integrated Test & Development Environment
Jin Wenrui;Zhan Xingqun
Jin Wenrui;Zhan Xingqun
..............page:56-60
Study on USB Gadget Driver Framework in Embedded Linux
Li Chuanwei;Hu Jinchun
Li Chuanwei;Hu Jinchun
..............page:51-55,60
Design of Robust Flight Control System Based on PID Controller
Su Bin;Chen Hongying
Su Bin;Chen Hongying
..............page:46-50
The SEU-tolerant System Design of Spacecraft Computer Based on COTS
Huang Ying;Zhang Chunyuan
Huang Ying;Zhang Chunyuan
..............page:40-45,50
A Circuit Design for Adaptive Synchronization of Chaotic Systems
Han Xinna;Li Zhi;Xi Bo;Zhu Li
Han Xinna;Li Zhi;Xi Bo;Zhu Li
..............page:36-39
A Model-independent Adaptive Variable-Structure Controller for Attitude Tracking
He Donglei;Cao Xibin
He Donglei;Cao Xibin
..............page:31-35
A Method to Improve the Stability of Formation Configuration by Adjustable Area-mass-ratio
Hao Jigang;Zhang Yulin
Hao Jigang;Zhang Yulin
..............page:27-30,35
..............page:23-26
Optimal Trajectories Design and Closed-loop Guidance Law Study for Aero-assisted Space Rendezvous
Chen Hongbo;Yang Di
Chen Hongbo;Yang Di
..............page:17-22,26
A Linear Quadratic Optimal Guidance Method for Lunar Soft Landing
Huang Xiangyu;Wang Dayi;Guan Yifeng
Huang Xiangyu;Wang Dayi;Guan Yifeng
..............page:11-16
Analysis of Extended and Unscented Kalman Filtering for INS/GPS Integration
Xu Huijuan;Wu Meiping;Luo Bing
Xu Huijuan;Wu Meiping;Luo Bing
..............page:7-10,16
Integrative Design of Terminal Maneuver and Self-guidance Phase for Anti-ship Missile
Wang Guangyuan;Zeng Jiayou;Sun Tao;Cong Hongri
Wang Guangyuan;Zeng Jiayou;Sun Tao;Cong Hongri
..............page:4-6,16
hang tian kong zhi de " da shi jian "
hou xiong
hou xiong
..............page:3