Modeling and Simulation of Rotor Dynamics of a Tilt-rotor Aircraft

被引：0
|
作者：
Sasongko, R. A. [1 ]
Muhammad, B. [1 ]
机构：
[1] Inst Teknol Bandung, Fac Mech & Aerosp Engn, Bandung, Indonesia
来源：
PROCEEDINGS OF 2017 5TH INTERNATIONAL CONFERENCE ON INSTRUMENTATION, COMMUNICATIONS, INFORMATION TECHNOLOGY, AND BIOMEDICAL ENGINEERING (ICICI-BME): SCIENCE AND TECHNOLOGY FOR A BETTER LIFE | 2017年
关键词：
dynamics; rotor; rotor blade; tilt-rotor; modeling;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
This paper provides a model of rotor dynamics which is derived mathematically and develops it into a numerical simulation model. The mathematical model was derived by reviewing the kinematic phenomena of a rotating blade and connected them with corresponding forces and moments working on the blade. The mathematical model was then developed into a numerical simulation model created in MATLAB Simulink environment. The model is based on a rotor mounted on a rotary wing aircraft with tilt-rotor configuration, which uses two rotors at both ends of its wings, with four blades each. The results of the simulation are used to analyze the characteristics and dynamics of a rotor and how they affect the flight dynamics of an aircraft.
引用
收藏
页码：51 / 56
页数：6
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