APPLICATION OF PRECOMPUTED CONTROL LAWS IN A RECONFIGURABLE AIRCRAFT FLIGHT CONTROL-SYSTEM

被引：78

作者：

MOERDER, DD

HALYO, N

BROUSSARD, JR

CAGLAYAN, AK

机构：

[1] INFORMAT & CONTROL SYST INC,HAMPTON,VA

[2] TEXAS INSTRUMENTS,LEWISVILLE,TX

[3] CHARLES RIVER ANALYT INC,CAMBRIDGE,MA

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1989年 / 12卷 / 03期

关键词：

D O I：

10.2514/3.20412

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：325 / 333

页数：9

共 13 条

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DOWNING, DR ;

BRYANT, WH .

AUTOMATICA, 1985, 21 (01) :23-34

[3]

CAGLAYAN A, 1987, AFWAL TR873024 AIR F

[4]

CHANDLER PR, 1984, SELF REPAIRING FLIGH

[5]

HALYO N, 1983, ICS TM83011

[6]

HALYO N, 1983, 1ST P ANN AIRCR CONT

[7]

HOWELL W, 1983, AUG P AIAA GUID CONT

[8] ROBUSTNESS RESULTS IN LINEAR-QUADRATIC GAUSSIAN BASED MULTIVARIABLE CONTROL DESIGNS [J].

LEHTOMAKI, NA ;

SANDELL, NR ;

ATHANS, M .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1981, 26 (01) :75-92

[9]

LOOZE D, 1985, NASA CR172489

[10]

Looze D. P., 1985, IEEE Control Systems Magazine, V5, P16, DOI 10.1109/MCS.1985.1104940

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