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
Reference:
Kubar,
S.V.
(2013),
"Syntez informatsiinykh dynamichnykh obraziv hranychnykh rezhymiv polotu vynyshchuvacha" ,
Science and Technology of the Air Force of Ukraine,
No.
4(13),
pp. 22-25.
УКР
