Active vibration control of aerospace structures using smart concept is one of the potential areas of application, the successful implementation of which requires design, development of instrumentation. electronics, digital signal processing techniques, computers, control system, robust control law, structure with built-in sensors and actuators coupled with good analytical and system identification studies, This paper essentially deals with some of the above issues and requirements. Further, it focuses on the design, development of instrumentation catering to piezos being used as sensors and actuators on the host structure to achieve active vibration control. The implementation of active vibration control for a single channel is explained in detail. The paper concludes with the description of adaptation of the above for multi-channel vibration control
