Разработка методов интенсификации резонансных режимов вывода из плоского штопора самолёта транспортной категории

Abstract

The problem of spin recovery for regional-category passenger aircraft is considered. The efficiency of resonans rocking technique for recovery from flat spin is demonstrated by the mathematical modeling. It is shown that disturbans of resonans by means of longitudinal control with variable frequency of elevator deflections is the most efficient for spin recovery, if the conventional standard “positional” technique fails.