Steering gear dynamic characteristics limits determination based on aircraft marginal flight modes

Aviation technics and technology


Аuthors

Bliznova T. B.1, Obolensky Y. G.2*, Polkovnikov V. A.3

1. MIG corporation, 6, Leningraskoe shosse, Moscow, 125171, Russia
2. Russian Aircraft Corporation MiG, 2, Leningradskoe shosse, Moscow, 125171, Russia
3. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: y.obolensky@rsk-mig.ru

Abstract

Main principles of modern steering gear dynamic characteristics limits determining are developed, using aircraft marginal flight modes, such as marginal overload and disposable roll rate. A new method of steering transmission mechanical characteristics calculating is presented.

Keywords:

limit dynamic characteristics; steering; aircraft maneuvering; marginal overload


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