FIELD: aviation.
SUBSTANCE: to produce a signal the identifying of the aircraft aerodynamic characteristics on the basis of the incidence angle recovery in a certain way, measured pitch angles, control displacement angles, pitch angular velocity, as well as normal acceleration. Stabilization loop gains of the aircraft longitudinal angular motion are adjusted, unmanned aerial vehicle longitudinal angular motion stabilization signal is formed on the basis of the adjusted coefficients.
EFFECT: required quality of the aircraft angular motion stabilization in a wide range of speeds and altitudes at perturbation effect.
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