OPTIMAL THRUST CONTROL OF A MISSILE WITH A PULSE MOTOR

被引：15

作者：

IMADO, F ^{[1
]}

KURODA, T ^{[1
]}

MIWA, S ^{[1
]}

机构：

[1] TOKYO DENKI UNIV,FAC ENGN,DEPT ELECT COMMUN ENGN,CHIYODA KU,TOKYO 101,JAPAN

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1991年 / 14卷 / 02期

关键词：

D O I：

10.2514/3.20649

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Optimal thrust control of a missile with a realistic pulse motor for midcourse guidance is proposed. First, the optimal thrust pattern that maximizes the missile's final velocity is calculated by solving a nonlinear two-point boundary value problem. Second, the way of implementing this pattern with a realistic pulse motor is studied. The result shows that the optimal thrust pattern is well approximated by a two-pulse type rocket motor. The optimization of the two-pulse control and the comparison with single-thrust control are studied and discussed.

引用

页码：377 / 382

页数：6

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