STOCHASTIC CONTROL OF F-8C AIRCRAFT USING A MULTIPLE MODEL ADAPTIVE-CONTROL (MMAC) METHOD .1. EQUILIBRIUM FLIGHT

被引：183

作者：

ATHANS, M ^{[1
]}

CASTANON, D ^{[1
]}

DUNN, KP ^{[1
]}

GREENE, CS ^{[1
]}

LEE, WH ^{[1
]}

SANDELL, NR ^{[1
]}

WILLSKY, AS ^{[1
]}

机构：

[1] MIT,DEPT ELECT ENGN & COMP SCI,ELECTR SYST LAB,CAMBRIDGE,MA 02139

来源：

关键词：

D O I：

10.1109/TAC.1977.1101599

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

引用

页码：768 / 780

页数：13

共 30 条

[1] AOKI M, 1976, OPTIMIZATION STOCHAS, P237
[2] ROLE AND USE OF STOCHASTIC LINEAR-QUADRATIC-GAUSSIAN PROBLEM IN CONTROL SYSTEM DESIGN
ATHANS, M
[J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1971, AC16 (06) : 529 - +
[3] ATHANS M, 1973, APR P S PAR EST TECH, P315
[4] ATHANS M, TO BE PUBLISHED
[5] ATHANS M, 1972, ANN ECONOMIC SOCIAL, V2, P449
[6] ATHANS M, 1975, 1975 P IEEE C DEC CO, P217
[7] ATHANS M, 1975, AUG P ENG F C SYST E
[8] DESPANDE JG, 1973, AUOMATICA, V9, P107
[9] NASAS ADVANCED CONTROL LAW PROGRAM FOR F-8 DIGITAL FLY-BY-WIRE AIRCRAFT
ELLIOTT, JR
[J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1977, 22 (05) : 753 - 757
[10] Etkin B., 1972, DYNAMICS ATMOSPHERIC, P134