FLEXIBLE SPACECRAFT ATTITUDE-CONTROL USING A SIMPLE P + D ALGORITHM

被引：0

|

作者：

FENTON, J

GILL, KF

机构：

来源：

AERONAUTICAL JOURNAL | 1981年 / 85卷 / 844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

收藏

页码：185 / 189

页数：5

相关论文

共 50 条

[1] ATTITUDE-CONTROL TEST OF FLEXIBLE SPACECRAFT
YAMASHITA, T
KURII, T
NEC RESEARCH & DEVELOPMENT, 1993, 34 (03): : 396 - 404
[2] ROBUST NONLINEAR ATTITUDE-CONTROL OF FLEXIBLE SPACECRAFT
SINGH, SN
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1987, 23 (03) : 380 - 387
[3] ATTITUDE-CONTROL SYSTEMS IN SPACECRAFT
KROSCHEL, NK
AUSTRALIAN JOURNAL OF INSTRUMENTATION & CONTROL, 1973, 29 (03): : 83 - 83
[4] MULTIAXIS TRACKING AND ATTITUDE-CONTROL OF FLEXIBLE SPACECRAFT WITH REACTION JETS
HABLANI, HB
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1994, 17 (04) : 831 - 839
[5] ROBUST BEAM-POINTING AND ATTITUDE-CONTROL OF A FLEXIBLE SPACECRAFT
YUAN, JSC
STIEBER, ME
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1986, 9 (02) : 228 - 234
[6] NONLINEAR ATTITUDE-CONTROL OF FLEXIBLE SPACECRAFT UNDER DISTURBANCE TORQUE
SINGH, SN
ACTA ASTRONAUTICA, 1986, 13 (08) : 507 - 514
[7] ATTITUDE-CONTROL OF TETHERED SPACECRAFT
LEMKE, LG
POWELL, JD
HE, XH
JOURNAL OF THE ASTRONAUTICAL SCIENCES, 1987, 35 (01): : 41 - 55
[8] FLEXIBLE SPACECRAFT MANEUVER - INVERSE ATTITUDE-CONTROL AND MODAL STABILIZATION
SINGH, SN
ACTA ASTRONAUTICA, 1988, 17 (01) : 1 - 9
[9] COMPENSATING STRUCTURE AND PARAMETER OPTIMIZATION FOR ATTITUDE-CONTROL OF A FLEXIBLE SPACECRAFT
CEBALLOS, DC
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1986, 9 (02) : 248 - 249
[10] OPTIMAL AERODYNAMIC ATTITUDE-CONTROL OF SPACECRAFT
PANDE, KC
VENKATACHALAM, R
ACTA ASTRONAUTICA, 1979, 6 (11) : 1351 - 1359

← 1 2 3 4 5 →