| 飞机起落架数学模型的研究 |
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| 引用本文： | 徐冬苓,李玉忍.飞机起落架数学模型的研究[J].系统仿真学报,2005,17(4):831-833. |
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| 作者姓名： | 徐冬苓 李玉忍 |
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| 作者单位： | 西北工业大学自动化学院,陕西西安,710072 |
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| 摘 要： | 对飞机起落架组成及工作原理进行较为详细的研究，建立了飞机起落架的数学模型，并在MATLAB／SIMULINK环境下进行系统仿真，给出仿真结果，分析了起落架对飞机防滑刹车系统的影响。仿真结果表明系统模型基本合理、正确，为设计、改进飞机防滑刹车系统，提高刹车效率和刹车性能，具有重要的指导意义。
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| 关 键 词： | 起落架 缓冲器 横向刚度 飞机防滑刹车系统 |
| 文章编号： | 1004-731X(2005)04-0831-03 |
| 修稿时间： | 2004年4月18日 |
Mathematical Model Research on Aircraft Landing Gear |
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| XU Dong-ling,LI Yu-ren.Mathematical Model Research on Aircraft Landing Gear[J].Journal of System Simulation,2005,17(4):831-833. |
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| Authors: | XU Dong-ling LI Yu-ren |
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| Abstract: | It is investigated the composition and the principle of the aircraft landing gears, and the model structure of it is set up. It is simulated in the MATLAB/SIMULINK, the result of the aircraft anti-skid system is also presented and the effect on the aircraft anti-skid system is analysed in details. The result shows that the aircraft landing gear system model established is basically rational andcorrect.Itishelpfultodesigntheaircraftanti-skidbrakingsystem,andtoimprovethebrakingefficiency andthebrakingperformance. |
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| Keywords: | landing gear damper stiffness aircraft anti-skid system |
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