Impact angle control over composite guidance law based on feedback linearization and finite time control

被引：3
|
作者：
Zhang Xiaojian [1 ]
Liu Mingyong [1 ]
Li Yang [1 ]
Zhang Feihu [1 ]
机构：
[1] Northwestern Polytech Univ, Sch Marine Sci & Technol, Xian 710021, Shaanxi, Peoples R China
来源：
JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS | 2018年 / 29卷 / 05期
基金：
中国国家自然科学基金;
关键词：
guidance law; impact angle; feedback linearization; finite time control; global stabilization; SLIDING-MODE GUIDANCE; STABILIZATION; INTERCEPTION; CONSTRAINT; STABILITY; DESIGN;
D O I：
10.21629/JSEE.2018.05.14
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The impact angle control over guidance (IACG) law against stationary targets is proposed by using feedback linearization control (FLC) and finite time control (FTC). First, this paper transforms the kinematics equation of guidance systems into the feedbackable linearization model, in which the guidance law is obtained without considering the impact angle via FLC. For the purpose of the line of sight (LOS) angle and its rate converging to the desired values, the second-order LOS angle is considered as a double-integral system. Then, this paper utilizes FTC to design a controller which can guarantee the states of the double-integral system converging to the desired values. Numerical simulation illustrates the performance of the IACG, in contrast to the existing guidance law.
引用
收藏
页码：1036 / 1045
页数：10
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