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

Aviation technics and technology


Аuthors

Shilova M. S.

PJSC “Sukhoi Company”, 23A, Polikarpova str., 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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