Steering gear dynamic characteristics limits determination based on aircraft marginal flight modes
Aviation technics and technology
Аuthors1, 2*, 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
AbstractMain 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