Command Filtered Adaptive Control for Integrated Missile Guidance and Autopilot with Terminal Angular Constraint

被引：0
|
作者：
Liang, Xiaoling [1 ]
Wang, Ning [1 ]
Liu, Yancheng [1 ]
Lv, Shuailin [1 ]
Xu, Bin [2 ]
机构：
[1] Dalian Maritime Univ, Marine Engn Coll, Dalian 116026, Peoples R China
[2] Northwestern Polytech Univ, Fremont, CA USA
来源：
PROCEEDINGS OF THE 2016 12TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA) | 2016年
关键词：
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：
For homing missiles considering terminal angular constraint, integrated design of guidance and control utilizing adaptive command filtered backstepping is studied in this paper. The proposed control scheme guarantees not only the stability of the missile dynamics with state constraints but also the interception performance with a desired terminal attitude angle. An adaptive law is introduced to compensate unknown uncertainties in the varying-time system. Simulation results are further presented to show the effectiveness and performance of the proposed approach.
引用
收藏
页码：715 / 720
页数：6
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