ANALYSIS OF AIRCRAFT ATTITUDE-CONTROL SYSTEMS PRONE TO PILOT-INDUCED OSCILLATIONS

被引：16

作者：

HESS, RA

机构：

来源：

关键词：

D O I：

10.2514/3.56363

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：106 / 112

页数：7

共 17 条

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POWERS, BG
SZALAI, KJ
WILSON, RJ
[J]. JOURNAL OF AIRCRAFT, 1982, 19 (04): : 318 - 323
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[7] HESS RA, 1980, AIAA801624 PAP
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[9] AN OPTIMAL CONTROL MODEL OF HUMAN RESPONSE .1. THEORY AND VALIDATION
KLEINMAN, DL
BARON, S
LEVISON, WH
[J]. AUTOMATICA, 1970, 6 (03) : 357 - &
[10] McRuer D., 1965, AFFDLTR6515