Active damping in HDD actuator

被引:37
作者
Huang, FY [1 ]
Semba, T
Imaino, W
Lee, F
机构
[1] IBM Almaden Res Ctr, San Jose, CA 95120 USA
[2] IBM Tokyo Res Lab, Tokyo, Japan
[3] IBM Japan Ltd, Tokyo Res Lab, Kanagawa, Japan
关键词
actuator; damping; dynamics; HDD; servo;
D O I
10.1109/20.917629
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
One of the limitations inherent in high-track density hard disk drive design is the effect of actuator mechanical resonant modes on the head-positioning servo. The first servo bandwidth limiting mode is the so-called "butterfly mode," which is the major mode in the head mechanical transfer functions and can not be avoided through mechanical design. A special active damping technique has been developed for rotary actuators of 3-1/2 " drives. With an additional sensor on the actuator and an external feedback loop, the butterfly mode can be damped and stiffened while the system stability is maintained. A theoretical system model, based on FEM, modal superposition and feedback control, is developed for analytical prediction of system stability and dynamics. Drive level experiments are conducted on actuators of two different designs, and show that the butterfly mode can be totally damped such that the gain of the head mechanical transfer function is close to 1/s(2). The end arm mode is also damped by about 8 dB for one actuator design, Servo improvement is also studied. It shows that the butterfly mode notch filter can be removed, and the phase margin can be improved by 7 degrees.
引用
收藏
页码:847 / 849
页数:3
相关论文
共 5 条
  • [1] HUANG F, 2000, Patent No. 6064540
  • [2] HUANG F, 1999, 10 ANN S INF STOR PR
  • [3] KOBAYASHI M, 1997, P INT C MICR INF PRE, P475
  • [4] Lee F., 2000, Japan Patent, Patent No. [JP3037946, 3037946]
  • [5] SIDMAN MD, 1995, Patent No. 5459383