ANALYSIS OF THE TECHNIQUE OF ROBUST EIGENSTRUCTURE ASSIGNMENT WITH APPLICATION TO AIRCRAFT CONTROL

被引:58
作者
MUDGE, SK
PATTON, RJ
机构
来源
IEE PROCEEDINGS-D CONTROL THEORY AND APPLICATIONS | 1988年 / 135卷 / 04期
关键词
D O I
10.1049/ip-d.1988.0038
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
引用
收藏
页码:275 / 281
页数:7
相关论文
共 15 条
[1]   DEVELOPMENT OF CONTROL LAWS FOR A FLIGHT TEST MANEUVER AUTOPILOT [J].
ALAG, GS ;
DUKE, EL .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1986, 9 (04) :441-445
[2]  
[Anonymous], 1980, MILF8785C
[3]  
DAzzo J. J., 1975, LINEAR CONTROL SYSTE, V3rd
[4]  
GAULT JD, 1968, J AIRCRAFT, V5
[5]  
Golub G. H., 2013, MATRIX COMPUTATIONS, V3
[6]   QUADRATIC WEIGHTS FOR ASYMPTOTIC REGULATOR PROPERTIES [J].
HARVEY, CA ;
STEIN, G .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1978, 23 (03) :378-387
[7]   ROBUST POLE ASSIGNMENT IN LINEAR STATE FEEDBACK [J].
KAUTSKY, J ;
NICHOLS, NK ;
VANDOOREN, P .
INTERNATIONAL JOURNAL OF CONTROL, 1985, 41 (05) :1129-1155
[8]  
McRuer D. T., 1973, AIRCRAFT DYNAMICS AU
[9]  
MIELKE RR, 1985, NASA3889 CONTR REP
[10]   FLEXIBILITY OFFERED BY STATE FEEDBACK IN MULTIVARIABLE SYSTEMS BEYOND CLOSED-LOOP EIGENVALUE ASSIGNMENT [J].
MOORE, BC .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1976, 21 (05) :689-692