On a certain approach to modeling aerodynamics and dynamics of spatial motion of single rotor helicopters


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Abstract

An approach that can be used for modeling the situation of unanticipated yaw is presented. A software is developed that allows us to obtain the helicopter equilibrium attitude at an arbitrary speed and consider the helicopter dynamics under influence of a certain disturbing factor.

About the authors

Yu. P. Onushkin

Russian Air Force Military Educational and Scientific Center “Air Force Academy named after N.E. Zhukovskii and Yu. A. Gagarin”, Syzran Branch

Email: sizov.syzran@gmail.com
Russian Federation, ul. Marshala Zhukova 1, Syzran, Samara oblast, 446007

D. A. Sizov

Samara State Technical University, Syzran Branch

Author for correspondence.
Email: sizov.syzran@gmail.com
Russian Federation, ul. Sovetskaya 45, Syzran, Samara oblast, 446001

V. A. Poluyakhtov

Russian Air Force Military Educational and Scientific Center “Air Force Academy named after N.E. Zhukovskii and Yu. A. Gagarin”, Syzran Branch

Email: sizov.syzran@gmail.com
Russian Federation, ul. Marshala Zhukova 1, Syzran, Samara oblast, 446007

V. G. Pidodnya

Samara State Technical University, Syzran Branch

Email: sizov.syzran@gmail.com
Russian Federation, ul. Sovetskaya 45, Syzran, Samara oblast, 446001

A. V. Ostrovoi

AO Center for Scientific and Technical Services “Dinamika”

Email: sizov.syzran@gmail.com
Russian Federation, ul. Shkol’naya 9/18, Zhukovsky, Moscow oblast, 140184

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