A helicopter with a helicopter rotary wing hub rotating at a helicopter operational rotation frequency and having a periodic vibration, said helicopter including a vibration control system, said vibration control system including at least a first motor with a first imbalance mass concentration, said first motor driving said first imbalance mass concentration with a first mass concentration phase and a first mass concentration speed and at least a second motor with a second imbalance mass concentration, said second motor driving said second imbalance mass concentration with a second mass concentration phase and a second mass concentration speed, said vibration control system controlling said first mass concentration phase, said first mass concentration speed, said second mass concentration phase and said second mass concentration speed to produce a rotating net force vector to inhibit said periodic vibration, with said first imbalance mass concentration opposingly oriented relative to said second imbalance mass concentration during a starting stopping rotation speed less than said first mass concentration speed and said second mass concentration speed.