| 基于能量法的舰载机拦阻着舰动力学分析及建模仿真 |
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| 引用本文： | 史红伟,徐元铭,刘博.基于能量法的舰载机拦阻着舰动力学分析及建模仿真[J].飞机设计,2011,31(6):1-5,15. |
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| 作者姓名： | 史红伟 徐元铭 刘博 |
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| 作者单位： | 北京航空航天大学航空科学与工程学院,北京,100191 |
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| 摘 要： | 针对舰载机拦阻着舰过程，采用能量法分析了任意着舰姿态和位置下的拦阻力响应，建立了全机六自由度动力学模型，考虑了航母甲板风的影响以及航母纵摇和升沉运动。通过MATLAB／SIMULINK建立数学模型，并以一种偏心非垂直着舰拦阻状态为算例进行了仿真分析。
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| 关 键 词： | 舰载机 拦阻着舰 能量法 计算机仿真 |
Dynamic Analysis and Computational Simulation for Aircraft Arrested Landing Based on Energy Method |
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| SHI Hong-wei,XU Yuan-ming,LIU Bo.Dynamic Analysis and Computational Simulation for Aircraft Arrested Landing Based on Energy Method[J].Aircraft Design,2011,31(6):1-5,15. |
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| Authors: | SHI Hong-wei XU Yuan-ming LIU Bo |
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| Institution: | ( School of Aeronautical Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China ) |
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| Abstract: | During the arrested landing process of carrier-based aircraft, the energy method is applied to analysis the performance of arresting force when aircraft is arrested at different initial posture and position, and the 6-DOF motion equations is built, also considering the carrier motions and deck wind. An example is studied under off-center and non-vertical condition based on mathematical model which is build by MATLAB/SIMULINK tool box. |
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| Keywords: | carrier-based aircraft arrested landing energy method computational simulation |
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