Home | Survey | Payment| Talks & Presentations | Job Opportunities
Journals   A B C D E F G H I J K L M N O P Q R S T U V W X Y Z
Aerospace Control
1006-3242
1992 Issue 4
The Proportional-Navigation Guidance Law for Leading of lmpact Point and its Realizing Method
Lu Yufeng;Shi Zhijia North-Western Polytechnical University
..............page:1-8+15
Synthesis of Flight Control Systems with Optimal Design Based on Reducing Trajectory Sensitivity
Liu Mingjun;Wu Dayou;Ma Hongxu Defence Science and Technology University Automatic Control Department
..............page:9-15
Research on the launching Method for Air-to-Ground Anti-Radiation Missiles
Liu Yinha;Chui Naigang;Liu Dun Harbin Institude of Technology
..............page:16-22+40
Applied Research of Antithetic Variable Sampling Method
Wu Liren Bejing Aerospace Automatic Control Institude
..............page:23-27
A Kalman filter for continuous alignment and calibration of the inertial platform
Zhang Zuiliang Institute of military operations research analysis
..............page:28-40
The Combined Laser Rader System as Measuring sensors for Complete Process of RVD in Space
Lin Laixing Beijing Institute of Control Engineering
..............page:41-48
Application of Differential GPS for Space Rendezvous
Lujun;Guo Jiong Space Science and Application Research Center;Chinese Academy of Sciences
..............page:49-55
Implementing and Analysing of Computer Aided Programming System(CAPS)
Zhang Bowen Beijing Aerospace Automatic Control Institute
..............page:56-60+68
Research and Design of Intelligent Control for Spacecrafts
Hong xin;Wu;Si Xiang;Yu Beijing Institute of Control Engineering
..............page:61-68
Missile-Borne Reduced Instruction Set Computers
Wang Qiaoyu Lishan Microelectronics Inst
..............page:69-74
The Trident Ⅱ Guidance System MK-6
Wang Xizhen Beijing Aerospace Automatic Control Institute
..............page:75-79