POWERED-FLIGHT TRAJECTORY OPTIMIZATION FOR AN INERTIAL-GUIDANCE BALLISTIC VEHICLE

被引：0
|
作者：
HOY, EC
LEONDES, CT
机构：
[1] TRW,SYST GRP,REDONDO BEACH,CA 90278
[2] UNIV CALIF,SCH ENGN & APPL SCI,LOS ANGELES,CA 90024
来源：
ASTRONAUTICA ACTA | 1972年 / 17卷 / 06期
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：857 / 870
页数：14
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