OPTIMAL CONTROL THEORIES IN DESIGN OF AIRCRAFT STABILITY AUGMENTATION AND CONTROL-SYSTEMS

被引：0

|

作者：

HEALEY, M ^{[1
]}

机构：

[1] UNIV COLL CARDIFF,ELECT & ELECTR ENGN DEPT,CARDIFF,WALES

来源：

MEASUREMENT AND CONTROL | 1974年 / 7卷 / 10期

关键词：

D O I：

10.1177/002029407400701006

中图分类号：

TH7 [仪器、仪表];

学科分类号：

0804 ; 080401 ; 081102 ;

摘要：

引用

收藏

页码：387 / 395

页数：9

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