Principles of Constructing the Systems of Restriction the Aircraft Critical Parameters


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Abstract

The problem on restriction of aircraft motion parameters is considered. Features of constructing the logical dynamic systems of critical parameters restriction for different channels of aircraft angular motion control are shown. The problems of synthesizing such systems are considered. The simulation results are presented.

About the authors

V. I. Petunin

Ufa State Technical University

Author for correspondence.
Email: petunin_vi@mail.ru
Russian Federation, ul. K. Marksa 12, Ufa, Bashkortostan, 450000

L. M. Neugodnikova

Ufa State Technical University

Email: petunin_vi@mail.ru
Russian Federation, ul. K. Marksa 12, Ufa, Bashkortostan, 450000


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