The transitional processes in fuzzy control systems of aircraft side movement

Аuthors

Repin A. I.^1*, Merkishin G. V.^**, Losev V. Y.²

1. Moscow State University of Engineering and Computer Science, 20, Stromynka str., Moscow, 107996, Russia
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: airepin@mail.ru
**e-mail: merkishingv@mail.ru

Abstract

Determinate and stochastic systems of automatic control are used for ensuring the safety of aircrafts flight. At good mete-vision (the 2-nd category ICAD and more) their usage is justified. For flying in more sophisticated conditions the known methods and tools do not juild the proper effect [1]. Then it is appropriate to employ the theory fuzzy control for designing such systems [2,3]. The article presents the structural scheme of the known control systems and systems based on the logical-linguistic approach. Their comparative characteristics are given. Then transition processes in the fuzzy system of automatic control for aircraft side movement are computer modeled.

Keywords:

determinate and stochastic systems, the theory fuzzy control, methods, the structural scheme