Comparative Analysis of Techniques of Modeling Kinematic Relations for Solving Helicopter Motion Equations

被引：0

作者：

Girfanov A.M. ^{[1
]}

机构：

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

来源：

Russian Aeronautics | 2018年 / 61卷 / 4期

关键词：

Euler angles; flight dynamics; helicopter; quaternions;

D O I：

10.3103/S1068799818040256

中图分类号：

学科分类号：

摘要：

This paper considers an aspect of selecting a technique of modeling kinematic relations that define angular speeds of rigid bodies and Euler angles as well as Rodrigues–Hamilton quaternions. © 2018, Allerton Press, Inc.

引用

页码：667 / 670

页数：3

共 6 条

[1]

Braverman A.S., Vaintrub A.P., Dinamika vertoleta. Predel'nye rezhimy poleta (Helicopter Dynamics. Limited Flight Conditions), (1988)

[2]

Leont'ev V.A., A Method for Determining Velocities and Accelerations of an Elastic Main Rotor Blade Element, Izv. Vuz. Av. Tekhnika, 53, 1, pp. 27-30, (2010)

[3]

Mikhailov S.A., Nedel'ko D.V., Nikolaev E.I., Mathematical Model of a Helicopter Landing with Skid Landing Gears, Izv. Vuz. Av. Tekhnika, 44, 1, pp. 8-12, (2001)

[4]

Mikhailov S.A., Girfanov A.M., Nedel'ko D.V., Metody matematicheskogo modelirovaniya rezhimov poleta i posadki vertoleta s bessharnirnym vintom (Methods of Mathematical Modeling of Flight and Landing Modes for a Helicopter with a Hingeless Rotor), (2016)

[5]

Encyclopedia of Mathematics, 1-5, (1977)

[6]

Girfanov A.M., Girfanova R.A., Numerical Modeling of Helicopter Flight on a Prescribed Trajectory, Izv. Vuz. Av. Tekhnika, 59, 3, pp. 40-44, (2016)

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