As an example, suppose a spacecraft equipped with two or more dual-gimbal CMGs experiences a transient unwanted torque, perhaps caused by reaction from venting waste gas, tending to make it roll clockwise about its forward axis and thus increase its angular momentum along that axis. Then the CMG control program will command the gimbal motors of the CMGs to slant the rotors' spin axes gradually more and more forward, so that the angular momentum vectors of the rotors point more nearly along the forward axis. While this gradual change in rotor spin direction is in progress, the rotors will be creating gyroscopic torques whose resultant is anticlockwise about the forward axis, holding the spacecraft steady against the unwanted waste gas torque.