Trajectory Tracking Method Based on Feedback Control in the Virtual Domain

被引:1
作者
Zhao Ji-guang [1 ]
Yan Liang [2 ]
Li Yuan [2 ]
Bai Guo-yu [2 ]
机构
[1] Acad Equipment, Sci Res Dept, Beijing 101416, Peoples R China
[2] Acad Equipment, Dept Sci Res, Beijing 101416, Peoples R China
来源
MECHATRONICS ENGINEERING, COMPUTING AND INFORMATION TECHNOLOGY | 2014年 / 556-562卷
关键词
Missile; Control theory; Nominal guidance law; Trajectory tracking; Interception; LINEARIZATION; VEHICLE;
D O I
10.4028/www.scientific.net/AMM.556-562.3246
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
A trajectory tracking method based on feedback control in the virtual domain is proposed for the algorithm of online real-time trajectory planning. The method using the way that polynomials approximate states and differential equations convert into algebraic equations. Time domain is converted into virtual domain by introducing the virtual path. Moreover, using the feedback correction tracks fixed trajectory exactly by real-time information. In the background of intercepting of ballistic missiles, simulation verification is carried out on the condition of initial minor disturbances. The simulation results demonstrate that the miss distance, pitch angle error and yaw angle error can meet the requirements.
引用
收藏
页码:3246 / +
页数:2
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