Modeling of helicopter flight imitation in the vortex ring state

被引：3

作者：

Toropov M.Y. ^{[1
]}

Stepanov S.Y. ^{[1
]}

机构：

[1] Tupolev Kazan National Research Technical University, ul. Karla Marksa 10, Kazan, Tatarstan

来源：

Russian Aeronautics | 2016年 / 59卷 / 4期

关键词：

flight simulator; helicopter; imitation modeling; vortex ring;

D O I：

10.3103/S1068799816040127

中图分类号：

学科分类号：

摘要：

A method of imitating the helicopter flight on a flight simulator is proposed for the vortex ring state hover flight. Algorithms of artificial neural networks are used for the modeling. The method allows modeling the characteristics of the main rotor's loading during a dangerous descent of the helicopter. © 2016, Allerton Press, Inc.

引用

页码：517 / 522

页数：5

共 5 条

[1]

Akimov A.I., Aerodinamika i letnye kharakteristiki, (1988)

[2]

Motsar' A.I., Determining the Regions of Vortex Ring Regimes of a Single-Rotor Helicopter Using Mathematical Modelling, in Otkrytye informatsionnye i komp’yuternye integrirovannye tekhnologii (Open Information and Computer Integrated Technologies), Kharkov: KHAI, pp. 5-20, (2009)

[3]

Girfanov A.M., Ledyankina O.A., Methodology of Using Artificial Neural Networks for Imitating the Loading of a Single-Rotor Helicopter, Izv. Vuz. Av. Tekhnika, 58, 4, pp. 26-30, (2015)

[4]

Gorban' A.N., Rossiev D.A., Neironnye seti na personal’nom komp’yutere, (1996)

[5]

Shcheglova V.M., Instability Flow of the Rotor on Modes of Sharp Descent and a Vortex Ring, Uchenye Zapiski TsAGI, 3, pp. 51-58, (2012)

← 1 →