For gyroscopic precession to occur, a moment has to be applied to the rotor disk. This does not appreciably happen by moving the fuselage or mast with a teetering rotor, or with other types.
A rigid rotor would have a moment applied by the fuselage rolling and/or pitching, but the amount of rotation added to the rotor disk is so small compared to it's existing roll that the effect would be difficult to observe.
Matthew.