TY - JOUR
T1 - Analysis of active vibration isolation system based on magnetostrictive actuator
AU - Zhang, Lei
AU - Liu, Yong Guang
AU - Fu, Yong Ling
AU - He, Lin
PY - 2004/12
Y1 - 2004/12
N2 - Based on the constitutive equation of magnetostrictive material, the model of the whole active vibration isolation system (AVIS) was put forward and its dynamics and stability of the control system were analyzed. Simulation results show that the parameters of the upper mass have much more influence on the active force of the actuator, and the stiffness of lower mass affects isolation performance while the absolute acceleration of middle mass is adopted as feedback. For the feedforward control scheme, system stability would not be influenced by the frequency variation, though the feedback link can reduce its stability margin. In the feedback control scheme, the time delay effect of the secondary path may cause the system unstable when the vibration frequency increases.
AB - Based on the constitutive equation of magnetostrictive material, the model of the whole active vibration isolation system (AVIS) was put forward and its dynamics and stability of the control system were analyzed. Simulation results show that the parameters of the upper mass have much more influence on the active force of the actuator, and the stiffness of lower mass affects isolation performance while the absolute acceleration of middle mass is adopted as feedback. For the feedforward control scheme, system stability would not be influenced by the frequency variation, though the feedback link can reduce its stability margin. In the feedback control scheme, the time delay effect of the secondary path may cause the system unstable when the vibration frequency increases.
KW - Active vibration isolation system
KW - Aerospace propulsion system
KW - Magnetostrictive actuator
KW - Modeling
KW - Stability of control system
UR - https://www.scopus.com/pages/publications/13444251166
M3 - 文章
AN - SCOPUS:13444251166
SN - 1000-8055
VL - 19
SP - 782
EP - 785
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 6
ER -