Continuous higher order sliding mode control with adaptation of air breathing hypersonic missile

被引：40
|
作者：
Yu, Polk [1 ]
Shtessel, Yuri [1 ]
Edwards, Christopher [2 ]
机构：
[1] Univ Alabama, Dept Elect & Comp Engn, 301 Sparkman Dr, Huntsville, AL 35899 USA
[2] Univ Exeter, Coll Engn Math & Phys Sci, Exeter, Devon, England
来源：
INTERNATIONAL JOURNAL OF ADAPTIVE CONTROL AND SIGNAL PROCESSING | 2016年 / 30卷 / 8-10期
关键词：
higher order sliding mode control; adaptive control; hypersonic missile control; OUTPUT-FEEDBACK CONTROL; VEHICLE;
D O I：
10.1002/acs.2664
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Hypersonic missile control in the terminal phase is addressed using continuous adaptive higher order sliding mode (AHOSM) control with adaptation. The AHOSM self-tuning controller is proposed and studied. The double-layer adaptive algorithm is based on equivalent control concepts and ensures non-overestimation of the control gain to help mitigating control chattering. The proposed continuous AHOSM control is validated via simulations of a hypersonic missile in the terminal phase. The robustness and high-accuracy output tracking in the presence of matched and unmatched external disturbances and missile model uncertainties is demonstrated. Copyright (C) 2016 John Wiley & Sons, Ltd.
引用
收藏
页码：1099 / 1117
页数：19
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