The long reach robots required for space applications necessitate acti
ve vibration control algorithms for a better pointing performance. The
inherent flexibility of the long and flexible space arms can generate
undesirable vibrations, making their end-point controls very difficul
t, although they provide a large reach volume and payload capabilities
. This paper presents a novel technique to control the vibrations of N
modes of a flexible link attached to a rigid robot employing an Imped
ance Control Technique using piezo-ceramic actuators and fiber-optic s
ensors. A piezo-ceramic actuator model has been developed by consideri
ng the moments/forces generated by the piezo-ceramic actuator as nonco
nservative external forces. Successful simulation and experimental res
ults have been obtained for vibration control of a cantilever beam whi
ch is attached to the end effector of the Titan-II robot arm.