The estimation procedure influence of hinge moment’s control surfaces to fighter’s dynamic characteristics.

Aviation technics and technology


Аuthors

Shilova M. S.

JSC «Sukhoi Company», 23B, Polikarpov str., p/b 604, Moscow, 125284, Russia

Abstract

It is engineered and applied the methodology estimate fighter’s dynamics data with a glance hinge moment’s action, created mathematical base and model «fighter – control system – hinge moment», defined flight zone.

Keywords:

estimation; hinge moment’s control surfaces; actuator; control system.


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