VIBRATION SUPPRESSION BY VARIABLE-STIFFNESS MEMBERS

被引:99
作者
ONODA, J
ENDO, T
TAMAOKI, H
WATANABE, N
机构
[1] NISSAN MOTOR CO LTD,DIV AEROSP,SUGINAMI KU,TOKYO 167,JAPAN
[2] INST SPACE & ASTRONAUT SCI,RES DIV SPACE TRANSPORTAT,KANAGAWA 229,JAPAN
关键词
D O I
10.2514/3.59943
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
An active vibration suppression concept, by varying the stiffness of a new type of variable-stiffness structural member, is proposed and investigated. The characteristics of this type of variable-stiffness system is shown to be different from previously studied types. The active vibration suppression with this type of variable-stiffness member is shown to be always stable. A theoretical investigation on a single-degree-of-freedom system shows potential high efficiency for this type of variable-stiffness system due to its unique hysteretic characteristics. Two different types of control logic are proposed for realistic multi-degree-of-freedom structures with multiple variable-stiffness members. Numerical simulations demonstrate the effectiveness of the proposed strategy. Active vibration suppression experiments of truss structures are performed by using a variable-stiffness member and the proposed control logic, demonstrating the effectiveness of the proposed technique in actual structures.
引用
收藏
页码:977 / 983
页数:7
相关论文
共 6 条
[1]  
CHEN GS, 1989, AIAA891327 PAP
[2]  
CHEN JC, 1984, J SPACECRAFT ROCKETS, V21, P4663
[3]  
CLARK WW, 1989, AIAA891330 PAP
[4]  
FANSON JL, 1989, AIAA891329 PAP
[5]  
NATORI M, 1988, 39TH C IAF BANG
[6]  
ONODA J, 1989, 40TH C IAF MAL