Lyapunov-based nonlinear missile guidance

被引：55
|
作者：
Léchevin, N
Rabbath, CA
机构：
[1] Univ Quebec, Dept Elect Engn, Trois Rivieres, PQ G9A 5H7, Canada
[2] Def Res & Dev Canada, Val Belair, PQ G3J 1X5, Canada
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2004年 / 27卷 / 06期
关键词：
D O I：
10.2514/1.8629
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A Lyapunov function candidate for the synthesis of nonlinear guidance laws was proposed. It was free of singularities, and for the stability analysis of missile-target systems considering the whole state. The proposed nonlinear guidance laws for three classes of target maneuvers were studied. For nonmaneuvering targets and targets having a constant acceleration, asymptotic stability was obtained and demonstrated.
引用
收藏
页码：1096 / 1102
页数：7
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