APPLICATION OF A NEW MULTIVARIABLE MODEL-FOLLOWING METHOD TO DECOUPLED FLIGHT CONTROL

被引：5

作者：

KANAI, K ^{[1
]}

UCHIKADO, S ^{[1
]}

NIKIFORUK, PN ^{[1
]}

HORI, N ^{[1
]}

机构：

[1] UNIV SASKATCHEWAN, MECH ENGN, SASKATOON S7N 0W0, SASKATCHEWAN, CANADA

来源：

关键词：

CONTROL-CONFIGURED-VEHICLE (CCV)-TYPE AIRCRAFT - DECOUPLED FLIGHT CONTROL - MODEL-FOLLOWING CONTROLLER;

D O I：

10.2514/3.20033

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：637 / 643

页数：7

共 6 条

[1]

Degawa T., 1982, Transactions of the Society of Instrument and Control Engineers, V18, P1132

ELLIOTT, H ;

WOLOVICH, WA .

FALB, PL ;

WOLOVICH, WA .

[4]

RIDGELY DB, 1983, AIAA830280 PAP

[5] INVARIANTS AND CANONICAL FORMS UNDER DYNAMIC COMPENSATION [J].

WOLOVICH, WA ;

FALB, PL .

SIAM JOURNAL ON CONTROL, 1976, 14 (06) :996-1008

[6]

WOLOVICH WA, 1974, LINEAR MULTIVARIABLE