
The methodology of the correct identification of the aerodynamic coefficients of the aircraft is considered, namely the determination of the partial derivatives of the aerodynamic forces and moments of the aircraft according to its state variables. The method of determining static (balancing) dependencies from short-term dynamic modes of a natural experiment is also presented. The effectiveness of the proposed approach is confirmed by the practice of determining the aerodynamic coefficients and aerodynamic characteristics of various aircraft.
нестаціонарність, ефективність, non-stationarity, correctness, літальні апарати, аеродинамічні коефіцієнти, коректність, non-linearity, efficiency, aerodynamic coefficients, ідентифікація, identification, active experiment, нелінійність, активний експеримент, aircraft
нестаціонарність, ефективність, non-stationarity, correctness, літальні апарати, аеродинамічні коефіцієнти, коректність, non-linearity, efficiency, aerodynamic coefficients, ідентифікація, identification, active experiment, нелінійність, активний експеримент, aircraft
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