Miniaturization and increased performance calculators, sensors and actuators are opening up the new possibilities of intelligent control complex mechatronic systems under the transient and turbulent conditions. Earlier adaptive control in a changing environment and with time-varying structure of the state space explored slightly due to the limited possibilities of practical implementation. The paper considers the model of an aircraft with a large number of sensors and actuators, distributed over surfaces of wings. In turbulent wind flows, it is shown that the multi-agent Local Voting Protocol with non-decreasing to zero step size allows equalization effects of disturbing forces acting on the different elements of wings.