The estimation procedure influence of hinge moment’s control surfaces to fighter’s dynamic characteristics.
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Aviation technics and technology
Аuthors
PJSC UAC Sukhoi Design Bureau, 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.Download