The 2nd order differential equations describing
the 3-DOF KCM system can be condensed into a matrix format as shown below:
Once
the component matrices for Mass, Stiffness, Damping and the Forcing Functions
are defined, the overall system can be further condensed into a matrix format
as:
Letters
in bold-italic are now vectors in matrix form. The response vectors and forcing
functions are single-column matrices, while the KCM ones are square. Working
with these matrices along the same lines as mentioned earlier, one can chop it
up into two first order ODE’s, which can be “matricized” as follows:
The
logic behind the above representation becomes fairly apparent when one expands
the matrices to two separate equations. To state the obvious, what was
originally a single set of matrix-equation in 2nd order has now doubled.
Performing
one last condensing, the above matrix then takes the form :
where
The
result is a matrix of 1st order ODE’s that can be numerically
integrated to obtain the solution of vector U. Such a representation of the system of 2nd order
equations is commonly referred to as the State-Space Method.
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