Modification of the design decisions in the statistical synthesis of the external characteristics of the aircraft

Аuthors

Balyk V. M.^*, Kulakova R. D.^**, Khesin L. B.

*e-mail: balikv@gmail.com
**e-mail: solnishko@mail.ru

Abstract

This paper investigates how to build and modify aerodynamic model unmanned aircraft based on flight tests. We give conditions for the stability of the design solution to the multicriteria and multi-factor uncertainties and statistical approach to the structural parametric synthesis of the aircraft.

Keywords:

the flying device, the statistical synthesis, project parameters.