Pneumatic suspensions, because of their significant advantages in comparison to classical suspension systems containing mechanical springs and hydraulic attenuators, are widely applied in road and railway vehicles. They also seem to be applicable in airplanes due to their advantageous impact properties. In this paper a simple one-wheel dynamical model of the pneumatic suspension is described. Impact properties of the model are studied in the context of the application in airplanes. Results of theoretical analysis and computer simulations are presented and compared with experimental data.
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