Aircraft Engineering
Аuthors
*, **, ***Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
*e-mail: Atovus@yandex.ru
**e-mail: naydenov.alexey@gmail.com
***e-mail: nselivanova2000@mail.ru
Abstract
This article reviews current state and prospects of the standalone drives. Reviewed contains a new actuator scheme which allows to achieve a high dynamic performance in standalone mode.Keywords:
actuator, self-contained, electro, hybrid, throttle, volume, electromotive, combined, control.
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