In this lecture, we will discuss about different strategies for active vibration control.
Different Strategies for vibration control:
Strategies (ii), (partly) (iv) and (v) are related to Active Vibration Control.
Applications of Active Vibration Control includes:
a. vibration and shape control of flexible systems like optical mirror
b. gitter control of high precision instruments
c. active suspension system for ride comfort in advanced vehicles
Application 1: Vibration & Shape Control of Optical Mirror
Active Control of Optical Aperture
This type of mirrors are ideally suitable for light weight ultra-large space telescopes. A set of such flexible mirror segments could be assembled to form the actual mirror. The surface quality is < 30nm. Stroke requirements for such adjustments is <2µm. Usually PZT actuators are bonded behind deformable silicon mirror membranes for this purpose. An electric field applied perpendicular to the piezoelectric layer plane will induce lateral contraction and thereby cause large out of plane deformation of the membrane.
Application 2: LSS: A future Interferometric Mission
Expanded view of the legs of a 6 DOF Isolator
For a 6 DOF active Isolator:
Active Vibration Control as shown in this diagram involves design of suitable vibration sensors, processing of sensory data and then feeding back necessary signal to the actuators for vibration control.
In a more abstract way the same could be depicted by a block diagram as shown here.
Figure: Block diagram of AVC system
where, r – reference signal, e – error signal, s-variable in the frequency domain, H – Transfer function of the sensor, G – Transfer function of the vibrating system, d- disturbance, Gc - Transfer function of the controller and y – output/response of the system.
Occasionally, if the nature of the disturbance is known then a feed-forward technique is adopted as shown here.
Special cases: Shunting of mechanical energy to electrical energy
This involves transformation of vibrational energy by the piezoelectric material and designing a suitable electrical network to dissipate this energy.
The piezoelectric patch is represented as a capacitor and a voltage source in series
Implementation of Controller: Inertial Actuator (Electro-mechanical System)
With the advent of new technologies, actuators and sensors are getting miniaturized and integrated to the structure. Thus, there is a transition from traditional active control to smart structure based active control. A case study of helicopter rotor vibration control will illustrate this.
Electro-Hydraulic Actuator
Smart Structural Control
Traditional active control can essentially control a finite number of vibrating modes of a continuous system. This may create instability due to the unwanted excitation of the higher modes. Smart structural control, on the other hand, is distributed in nature. It consumes less energy, gurantees stability and could be integrated easily to the vibrating body.
Comparison between two methods of AVC
Important issues related to AVC
Reference