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Improvement of handling qualities for the aircraft longitudinal motion


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Abstract

In this paper, we consider a task of efficiency improvement for the aircraft flight altitude stabilization by the nonlinear effects in control laws and angle of attack limiting.

About the authors

V. I. Garkushenko

Tupolev Kazan National Research Technical University

Author for correspondence.
Email: vigark@yandex.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111

S. S. Vinogradov

Tupolev Kazan National Research Technical University

Email: vigark@yandex.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111

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