Mathematical model and optimization of helicopter vertical takeoff considering operational conditions and aerodynamic damping

A mathematical model of helicopter vertical takeoff was created. The model takes into account operating conditions and individual performance capabilities of a given helicopter. An optimization technique based on a genetic algorithm was introduced. The influence of mass, initial height and outside a...

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Bibliographic Details
Main Authors: Yu. P. Onushkin, D. A. Sizov, V. A. Poluyakhtov, A. V. Ostrovoy
Format: Article
Language:English
Published: Samara National Research University 2017-11-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/5231/5083