MISSILE GUIDANCE BASED ON WEIGHT ADJUSTED SINGULAR PERTURBATION

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作者：
YOO, SH
BULLOCK, TE
机构：
来源：
AIAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE, PTS 1 AND 2: A COLLECTION OF TECHNICAL PAPERS | 1989年
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V [航空、航天];
学科分类号：
08 ; 0825 ;
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页码：496 / 503
页数：8
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