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

Аuthors

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

1. MIG corporation, 6, Leningraskoe shosse, Moscow, 125171, Russia
2. 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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