Rotordynamic analyses of large steam turbine-generators are very challenging tasks. Problems of huge amount of elements occur in modeling the multiple-bladed-disk rotors. However, from the viewpoints of rotordynamics, the major concern is on the vibration of rotating shafts and the models of the bladed disks need to be reduced. A modified pseudo mode shape method was proposed to reduce the models of bladed-disks in this study. The frequency response functions of bladed-disks obtained at the joints with the shafts are used to derive the condensed mass, damping, and stiffness matrices for the bladed-disks. This paper extends the theory of pseudo mode shape method developed previously to include rigid body modes and deformation modes of the bladed-disks. The feasibility and effectiveness of the extended pseudo mode shape method are justified by using a solid-modeled shaft and bladed disk as example.