MODERN CONTROL-THEORY FOR DESIGN OF AUTOPILOTS FOR BANK-TO-TURN MISSILES

被引:48
作者
WILLIAMS, DE [1 ]
FRIEDLAND, B [1 ]
MADIWALE, AN [1 ]
机构
[1] MIT,LINCOLN LAB,LEXINGTON,MA 02173
关键词
D O I
10.2514/3.20228
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:378 / 386
页数:9
相关论文
共 11 条
[1]  
ARROW A, 1983, NASACR3644
[2]  
BARRETT MF, 1980, DEC P IEEE C DEC CON, P885
[3]   ROBUSTNESS WITH OBSERVERS [J].
DOYLE, JC ;
STEIN, G .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1979, 24 (04) :607-611
[4]  
EMMERT RI, 1972, AFATLTR7810 AIR FORC
[5]  
Friedland B., 1986, CONTROL SYSTEM DESIG
[6]  
FRIEDLAND B, 1986, JUN P AM CONTR C SEA, P623
[7]   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
[8]  
RIGGS TL, 1981, AFATLTR8156 AIR FORC
[9]   GAIN AND PHASE MARGIN FOR MULTILOOP LQG REGULATORS [J].
SAFONOV, MG ;
ATHANS, M .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1977, 22 (02) :173-179
[10]  
SAFONOV MG, 1981, DEC P IEEE C DEC CON, P1472