A technique of structural design optimization for flying vehicle considering control system

Аuthors

Parafes S. G.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

e-mail: s.parafes@mail.ru

Abstract

A technique is offered to optimize structural design for flying vehicle into account control system. This technique uses a model of elastic dynamical system as a reference one. The reference model describes optimal mass and stiffness distributions for vehicle airframe units based on functional constraints due to interference of vehicle structure and control system. The technique offered is tested by solving structural optimization problem for unmanned airborne vehicle with aerodynamic controls.

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