Module 2: Active Vibration Control of Smart Composite Plate
  Lecture 22: Active Control of Damping
 

Response of a General Dynamic System

The equation of motion for a general dynamical system is in the form

(22.3)

The matrix C is arbitrary and may not be symmetric. The system must be treated as a general one. It is assumed that M and K are positive definite.

Introducing the 2n- dimensional state vector and the 2n-dimensional excitation vector, Equation (22.2) can be transformed into

(22.4)

and are real matrices. is a positive definite symmetric matrix. is neither positive definite nor symmetric.

Equation (22.4) can be rendered into a more convenient form by the Cholesky decomposition

(22.5)

Then, introducing the linear transformation

(22.6)

(22.7

where = ( ) =

Equation (22.5) can be reduced to

(22.8)

in which is a real non symmetrical matrix and is a real vector.

Since this is a free vibration case, , Hence, Equation (22.7) reduces to

(22.9)

The solution of Equation (22.8) may be expressed as

(22.10)

The final response may be obtained from Equation (22.9)

(20.11)