Dimensional measurements obtained with Coordinate Measuring Machines (CMMs)
are negatively affected by self-induced structural vibrations. In this pap
er a control strategy that reduces the structural vibrations in a CMM is ou
tlined and experimentally demonstrated. The control strategy, designated th
e Feedforward Filter, is developed by establishing the relationship between
contemporary controller input shaping techniques and traditional notch fil
tering methods. Issues on both robustness and multiple mode vibrations are
addressed. Controller input development takes place in the discrete time do
main. This method provides results identical to those for optimal command i
nput preshaping obtained through non-linear programming methods and require
s considerably less computational effort. Experimental results show a 50 pe
r cent reduction in the peak-to-peak magnitude of structural vibrations as
compared to unshaped bang-bang trajectories.