DYNAMICS OF A CANTILEVER BEAM ATTACHED TO A MOVING BASE

被引:537
作者
KANE, TR [1 ]
RYAN, RR [1 ]
BANERJEE, AK [1 ]
机构
[1] LOCKHEED MISSILES & SPACE CO INC,SUNNYVALE,CA 94086
关键词
D O I
10.2514/3.20195
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:139 / 151
页数:13
相关论文
共 40 条
[11]  
HEINS CP, 1976, BENDING TORSIONAL DE, P8
[12]   DEVELOPMENT OF DYNAMICS AND CONTROL SIMULATION OF LARGE FLEXIBLE SPACE SYSTEMS [J].
HO, JYL ;
HERBER, DR .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1985, 8 (03) :374-383
[13]   DIRECT PATH METHOD FOR FLEXIBLE MULTI-BODY SPACECRAFT DYNAMICS [J].
HO, JYL .
JOURNAL OF SPACECRAFT AND ROCKETS, 1977, 14 (02) :102-110
[14]   PROPER DEFINITION OF CURVATURE IN NONLINEAR BEAM KINEMATICS [J].
HODGES, DH .
AIAA JOURNAL, 1984, 22 (12) :1825-1827
[15]  
Hughes P. C., 1973, 24 C INT ASTR FED BA
[16]   MULTI-BODY DYNAMICS INCLUDING THE EFFECTS OF FLEXIBILITY AND COMPLIANCE [J].
HUSTON, RL .
COMPUTERS & STRUCTURES, 1981, 14 (5-6) :443-451
[17]  
KANE TR, 1983, SPACECRAFT DYNAMICS, P425
[18]  
KANE TR, 1985, DYNAMICS THEORY APPL, P24
[19]   EFFECTS OF WARPING AND PRETWIST ON TORSIONAL VIBRATION OF ROTATING BEAMS [J].
KAZA, KRV ;
KIELB, RE .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1984, 51 (04) :913-920
[20]   NONLINEAR FLAP-LAG-AXIAL EQUATIONS OF A ROTATING BEAM [J].
KAZA, KRV ;
KVATERNIK, RG .
AIAA JOURNAL, 1977, 15 (06) :871-874