Adding a Power Integrator Technique Based Terminal Guidance Law

被引：0
|
作者：
Wang, Songyan [1 ]
Sun, Xiangyu [1 ]
Chao, Tao [1 ]
Ma, Ping [1 ]
机构：
[1] Harbin Inst Technol, Control & Simulat Ctr, Harbin 150080, Peoples R China
来源：
2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2016年
基金：
中国博士后科学基金; 中国国家自然科学基金;
关键词：
NONLINEAR-SYSTEMS; TACTICAL MISSILES; AUTOPILOT DESIGN; STABILIZATION; FEEDBACK;
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：
In this paper a novel terminal guidance law for hypersonic vehicle is investigated. In order to accelerate the convergence rate of line of sight angle, adding a power integrator technique based nonlinear guidance law which can make the line of sight converge to zero in finite time is proposed. Then rigorous stability analysis of finite-time convergence is shown. It demonstrates the effectiveness of the approach by numerical simulation meanwhile the approach have strong robustness in the presence of disturbance.
引用
收藏
页码：2053 / 2057
页数：5
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