CONJUGATE GRADIENT METHOD AND ITS APPLICATION TO AEROSPACE VEHICLE GUIDANCE AND CONTROL .2. MARS ENTRY GUIDANCE AND CONTROL

被引：0

作者：

LEONDES, CT

WU, CA

机构：

[1] UNIV CALIF,LOS ANGELES,CA 90024

[2] UNIV WYOMING,LARAMIE,WY 82070

来源：

ASTRONAUTICA ACTA | 1972年 / 17卷 / 06期

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：881 / 890

页数：10

共 17 条

[1]

BREAKWELL JV, 1963, SIAN J CONTR, P193

[2] GUIDANCE SCHEME FOR SUPERCIRCULAR RE-ENTRY OF A LIFTING VEHICLE [J].

BRYSON, AE ;

DENHAM, WF .

ARS JOURNAL, 1962, 32 (06) :894-898

[3]

BRYSON AE, 1961, DETERMINATION LIFT D

[4]

BRYSON AE, 1961, NOV P S VEH SYST OPT

[5]

DOUGHERTY HJ, 1967, JOINT AUTOMATIC CONT, P125

[6]

Gelfand I., 1963, CALCULUS VARIATIONS

[7]

JOHNSON RW, 1966, THESIS UCLA

[8] CONJUGATE GRADIENT METHOD FOR OPTIMAL CONTROL PROBLEMS [J].

LASDON, LS ;

MITTER, SK ;

WAREN, AD .

[9]

LASDON LS, 1967, JACC P PHILADELPHIA, P538

[10]

MCLELLAN CH, 1967, J SPACECRAFT ROCKETS, V4, P164