QUATERNION FEEDBACK FOR SPACECRAFT LARGE-ANGLE MANEUVERS

被引：285

作者：

WIE, B

BARBA, PM

机构：

[1] Ford Aerospace & Communications, Corp, Systems Analysis Dep, Palo, Alto, CA, USA, Ford Aerospace & Communications Corp, Systems Analysis Dep, Palo Alto, CA, USA

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1985年 / 8卷 / 03期

关键词：

D O I：

10.2514/3.19988

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：360 / 365

页数：6

共 21 条

[1] SATELLITE ATTITUDE ACQUISITION BY MOMENTUM-TRANSFER [J].

BARBA, PM ;

AUBRUN, JN .

AIAA JOURNAL, 1976, 14 (10) :1382-1386

[2]

BRECKENRIDGE WG, 1983, AUG AAS AIAA ASTR SP

[3]

BRYSON AE, 1983, STABILIZATION CONTRO

[4]

CANNON RH, 1967, DYNAMICS PHYSICAL SY, P355

[5]

CUNNINGHAM DC, 1978, P AIAA GUIDANCE CONT

[6]

D'Amario L. A., 1979, Journal of Guidance and Control, V2, P339, DOI 10.2514/3.55885

[7]

HRASTAR J, 1970, NASA TN D5959

[8] A NEW METHOD FOR PERFORMING DIGITAL CONTROL SYSTEM ATTITUDE COMPUTATIONS USING QUATERNIONS [J].

ICKES, BP .

AIAA JOURNAL, 1970, 8 (01) :13-&

[9]

KANE TR, 1983, SPACECRAFT DYNAMICS

[10]

MARGULIES G, 1963, 52 PHILC W LAB MATH

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