Design of a three-dimensional CLOS guidance law via sliding mode control

被引：0
|
作者：
Cai, Peng [1 ]
Wang, Qing-Chao [1 ]
机构：
[1] Harbin Institute of Technology, Harbin 150001, China
来源：
Yuhang Xuebao/Journal of Astronautics | 2007年 / 28卷 / 06期
关键词：
Attitude control - Computer simulation - Degrees of freedom (mechanics) - Nonlinear systems;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
This paper design a new three-dimensional command line-of-sight (CLOS) guidance law via sliding mode control, which based on a six degrees of freedom flight model. The main idea lies in converting the three-dimensional CLOS guidance problem to the tracking problem of a time-varying nonlinear system. With the new design of tracking error, a new CLOS sliding mode guidance law was proposed. Through computer simulation, we investigate the guidance performance of our CLOS sliding mode guidance law.
引用
收藏
页码：1651 / 1655
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