a model for simulating the dynamics of the aircraft in the u0430u043fu0435u0440u0438u043eu0434u0438u0447u0435u0441u043au043eu043c rapid longitudinal movement with the base with attached thereto and a model plane with the ball. u043du0441u0438u0440u043eu0432u043eu0447u043du044bu043c control, which has u0434u0435u043cu043fu0444u0435u0440u043eu043c and spring with a thread attached clamp to the model plane, and the clamp is installed in the respective of the status of the aircraft aerodynamic, characterized by the fact thatwith the purpose of approaching the conditions of the simulation to the real, it is fitted with a platform from the angles of attack and pitch and telescopic u0448u0430u0440u043du0438u0440u043du043e connected to the t, heat a load on one shoulder and the air speed, while the other shoulder bars through the auxiliary damper which is connected with the bara model plane in the center of gravity of the u0448u0430u0440u043du0438u0440u043du043e connected with a telescopic rod and a platform that is connected through springs and u0434u0435u043cu043fu0444u0435u0440u0430 with the tail part of the mo with the plane, and through two series connected u043fu0430u0440u0430u043bu043bu0435u043bu043eu0433u0440u0430u043cu043cu043du044bu0445 mechanism with the bar.
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