The integrated information model is proposed and current limit modes of flight fighter that reduces a multi-dimensional domain limits of flight parameters to images of restrictions in the coordinates: airspeed - angular velocity of rotation in the horizontal and vertical planes. The problem of building quality-shaped interface using the description of dynamic systems characteristic surfaces, which allow to take into account the performance characteristics and features of the fighter extreme flight condition, such as cross-linking caused by the interaction of lateral and longitudinal channels in the process of changing the parameters and time-dependent components of the aerodynamic coefficients is considered in the article.
Keywords:
limiting modes of flight, information model, quality-shaped interface
УКР
