Active Vibration Suppression of a Nonlinear Flexible Spacecraft

M. Malekzadeh

Volume 11, Issue 1 , June 2017

Abstract
  In this article, the issue of attitude control and active vibration suppression of a nonlinear flexible spacecraft is assessed through piezoelectric patches as actuator and sensors. Two controller loops are applied: the inner loop, to make the panel vibration damped through piezoelectric patches; and ...  Read More