OPTIMAL NONLINEAR FEEDBACK-CONTROL FOR SPACECRAFT ATTITUDE MANEUVERS

被引：58

作者：

CARRINGTON, CK ^{[1
]}

JUNKINS, JL ^{[1
]}

机构：

[1] VIRGINIA POLYTECH INST & STATE UNIV,ENGN SCI & MECH,BLACKSBURG,VA 24061

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1986年 / 9卷 / 01期

关键词：

discussions of this work with Dr. S.R. Vadali. This work was supported by the Air Force Office of Scientific Research under Contract F4920-83-K-0032; the authors appreciatethe support and capable technical liasion of Dr. Anthony K. Amos of AFOSR;

D O I：

10.2514/3.20073

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：99 / 107

页数：9

共 13 条

[1]

CARRINGTON CK, 1984, J ASTRONAUT SCI, V32, P29

[2] NON-LINEAR OPTIMAL FEEDBACK-REGULATION OF SATELLITE ANGULAR MONENTA [J].

DABBOUS, TE ;

AHMED, NU .

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1982, 18 (01) :2-10

[3]

DWYER TAW, 1982, 21ST IEEE C DEC CONT

[4]

HOFFMAN HC, 1981, AIAA811760 PAP

[5]

JUANG JN, 1983, AASAIAA83375 PAP

[6]

Kirk DE., 2004, OPTIMAL CONTROL THEO

[7] PERTURBATION FORMULATIONS FOR SATELLITE ATTITUDE DYNAMICS [J].

KRAIGE, LG ;

JUNKINS, JL .

CELESTIAL MECHANICS, 1976, 13 (01) :39-64

[8]

LEE EB, 1967, F OPTIMAL CONTROL TH

[9] MATRIX QUADRATIC SOLUTIONS [J].

POTTER, JE .

SIAM JOURNAL ON APPLIED MATHEMATICS, 1966, 14 (03) :496-&

[10]

TURNER JD, 1982, AIAA821589 PAP

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