Approbation of a Mathematical Model of a Specialized Mechatronic System

The paper discusses a procedure for studying the adequacy of a nonlinear non-stationary aerodynamic model. The possibility for balancing and the stability of the balanced model in the altitude-speed range of operation of the real aircraft has been studied. The purpose of the research is to determine the range of altitudes and flight speeds in which the behavior of the object and the model coincide.