MISSILE GUIDANCE BASED ON WEIGHT ADJUSTED SINGULAR PERTURBATION

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作者：

YOO, SH

BULLOCK, TE

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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];

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08 ; 0825 ;

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页码：496 / 503

页数：8

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