Flight Dynamics Model of Helicopter Based on Simulink
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- 英文论文题名：Flight Dynamics Model of Helicopter Based on Simulink
- 论文作者：Shen'ao Yan ; Weihong Wang ; Sentang Wu ; Ke Lu
- 英文论文作者：Shen'ao Yan ; Weihong Wang ; Sentang Wu ; Ke Lu ; School of Automation Science and Electrical Engineering ; Beihang University ; Science and Technology on Aircraft Control Laboratory ; Beihang University ; Science and Technology on Rotorcraft Aeromechanics Laboratory
- 年：2017
- 作者机构：School of Automation Science and Electrical Engineering,Beihang University;Science and Technology on Aircraft Control Laboratory,Beihang University;Science and Technology on Rotorcraft Aeromechanics Laboratory;
- 英文论文关键词：Helicopter ; simulation model ; Simulink ; modeling
- 会议召开时间：2017-07-26
- 会议录名称：第36届中国控制会议论文集（B）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（B）
- 语种：英文
- 分类号：V212.4
- 学会代码：KZLL
- 会议名称：第36届中国控制会议
- 会议地点：中国辽宁大连
- 主办单位：中国自动化学会控制理论专业委员会
- 学会名称：中国自动化学会控制理论专业委员会
- 页数：5
- 文件大小：3777k
- 原文格式：D
- 会议级别：全国
摘要
In this paper, a complete numerical simulation model of helicopter flight dynamics was established. The modeling of the main aerodynamic components of the helicopter and the aerodynamic interference are taken into account, and the modeling methods of the airfoil aerodynamic model, the induced velocity model and the waving movement model are discussed in detail. Based on the hierarchical and modular modeling principles, the whole simulation model is finally realized on the Simulink platform. Finally, the model helicopter data are used to prove the rationality and validity of the modeling theory and method.
In this paper, a complete numerical simulation model of helicopter flight dynamics was established. The modeling of the main aerodynamic components of the helicopter and the aerodynamic interference are taken into account, and the modeling methods of the airfoil aerodynamic model, the induced velocity model and the waving movement model are discussed in detail. Based on the hierarchical and modular modeling principles, the whole simulation model is finally realized on the Simulink platform. Finally, the model helicopter data are used to prove the rationality and validity of the modeling theory and method.
In this paper, a complete numerical simulation model of helicopter flight dynamics was established. The modeling of the main aerodynamic components of the helicopter and the aerodynamic interference are taken into account, and the modeling methods of the airfoil aerodynamic model, the induced velocity model and the waving movement model are discussed in detail. Based on the hierarchical and modular modeling principles, the whole simulation model is finally realized on the Simulink platform. Finally, the model helicopter data are used to prove the rationality and validity of the modeling theory and method.
引文
[1]Yang Hongliang.An unmanned helicopter flight simulation dynamics modeling and program development[D].Shenyang University of Aeronautics and Astronautics,2016.
[2]Sun Wenda.Nonlinear modeling and control of small unmanned helicopter[D].Zhejiang University,2014.
[3]Wu Wenhai,Xu Li,Wang Qi.Study on Modeling and Robust Flight Control of Small Unmanned Helicopter[J].Aircraft Design,2014,(03):43-48.
[4]Chen Xianxiang,Liu Ying,Hu Xiongwen,Qian Yi,Wang Jinhua.Modeling and attitude control of micro-unmanned helicopter[J].Measurement and Control Technology,2014,(03):86-89.
[5]Ding Chunlong.Three-degree-of-freedom helicopter modeling and control method[D].Harbin University of Science and Technology,2014.
[6]Wu Wenhai,Xu Li,Wang Qi.Study on Modeling and Robust Control of Small Unmanned Helicopter[J].Flying Mechanics,2013,(06):526-529+534.
[7]Chen R T N.A Simplified Rotor System Mathematical Model for Piloted Flight Dynamics Simulation[R].NASA-TM-78575,1979.
[8]Howlett J J.UH-60A Black Hawk Engineering Simulation Program Volume-Mathematical Model[R].NASA CR-166309,1981.
[9]Chen R T N.A Simplified Rotor System Mathematical Model for Piloted Flight Dynamics Simulation[R].NASA-TM-78575,1979.
[10]Howlett J J.UH-60A Black Hawk Engineering Simulation Program–Volume-Mathematical Model[R].NASA CR-166309,1981.
[11]DuV al R.A Real-Time Blade Element Helicopter Simulation forH andling Qualities Analysis[C]//Proceedings of the 15th Annual European Rotorcraft Forum,Amsterdam,The Netherlands,1989.
[2]Sun Wenda.Nonlinear modeling and control of small unmanned helicopter[D].Zhejiang University,2014.
[3]Wu Wenhai,Xu Li,Wang Qi.Study on Modeling and Robust Flight Control of Small Unmanned Helicopter[J].Aircraft Design,2014,(03):43-48.
[4]Chen Xianxiang,Liu Ying,Hu Xiongwen,Qian Yi,Wang Jinhua.Modeling and attitude control of micro-unmanned helicopter[J].Measurement and Control Technology,2014,(03):86-89.
[5]Ding Chunlong.Three-degree-of-freedom helicopter modeling and control method[D].Harbin University of Science and Technology,2014.
[6]Wu Wenhai,Xu Li,Wang Qi.Study on Modeling and Robust Control of Small Unmanned Helicopter[J].Flying Mechanics,2013,(06):526-529+534.
[7]Chen R T N.A Simplified Rotor System Mathematical Model for Piloted Flight Dynamics Simulation[R].NASA-TM-78575,1979.
[8]Howlett J J.UH-60A Black Hawk Engineering Simulation Program Volume-Mathematical Model[R].NASA CR-166309,1981.
[9]Chen R T N.A Simplified Rotor System Mathematical Model for Piloted Flight Dynamics Simulation[R].NASA-TM-78575,1979.
[10]Howlett J J.UH-60A Black Hawk Engineering Simulation Program–Volume-Mathematical Model[R].NASA CR-166309,1981.
[11]DuV al R.A Real-Time Blade Element Helicopter Simulation forH andling Qualities Analysis[C]//Proceedings of the 15th Annual European Rotorcraft Forum,Amsterdam,The Netherlands,1989.