Flight guidance and control of a winged rocket

被引：0
|
作者：
Shimozawa, Tomoaki [1 ]
Sagara, Shinichi [1 ]
Narumi, Tomohiro [1 ]
Yonemoto, Koichi [1 ]
机构：
[1] Kyushu Inst Technol, Dept Mech & Control Engn, Kitakyushu, Fukuoka 8048550, Japan
来源：
PROCEEDINGS OF THE SEVENTEENTH INTERNATIONAL SYMPOSIUM ON ARTIFICIAL LIFE AND ROBOTICS (AROB 17TH '12) | 2012年
关键词：
Adaptive Control; Flight Control;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Since Reusable Launch Vehicles (RLVs) operate in a wide range of flight conditions, the values of the parameters of the RLVs' dynamic equations are not constant. Therefore, some adaptive control methods for RLVs have been proposed. We have proposed a digital adaptive feedback linearization control method with time-scale separation to a winged rocket. In this paper, we propose a digital adaptive feedback linearization control method using unscented Kalman filter. The simulation results with a guidance using genetic algorithm show the effectiveness of the proposed control systems.
引用
收藏
页码：65 / 68
页数：4
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