Sliding mode based impact angle guidance law considering actuator fault

被引:8
|
作者
He, Shaoming [1 ]
Lin, Defu [1 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
来源
OPTIK | 2015年 / 126卷 / 20期
关键词
Sliding mode control; Guidance law; Impact angle; Chattering-free; Actuator fault; PROPORTIONAL NAVIGATION; DESIGN;
D O I
10.1016/j.ijleo.2015.05.129
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
In this paper, a new continuous impact angle constraint guidance law in the presence of actuator fault is presented based on sliding mode control theory. The robustness and finite-time convergence of the basic guidance law is established using Lyapunov stability theory. For actuator compensation, an additional term is augmented in the original guidance law to guarantee finite-time stability of the closed-loop guidance system. Theoretical analysis and simulation results demonstrate the effectiveness of the proposed method. (C) 2015 Elsevier GmbH. All rights reserved.
引用
收藏
页码:2318 / 2323
页数:6
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