| 起落架载荷的自校正控制 |
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| 引用本文： | 贾玉红,刘鹰.起落架载荷的自校正控制[J].航空学报,2004,25(3):237-241. |
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| 作者姓名： | 贾玉红 刘鹰 |
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| 作者单位： | 北京航空航天大学,飞行器设计与应用力学系,北京,100083;北京航空航天大学,飞行器设计与应用力学系,北京,100083 |
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| 摘 要： | 通过建立自校正控制起落架的非线性模型和系统的ARMAX模型,对控制器进行了设计,并结合参数辨识,实现了起落架的自校正控制。计算机仿真结果表明,此方案有效地改善了飞机起落架的缓冲性能。
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| 关 键 词： | 起落架 滑行载荷 非线性模型 参数辨识 自校正控制 |
| 文章编号： | 1000-6893(2004)03-0237-05 |
| 收稿时间： | 2003-05-09 |
| 修稿时间： | 2003年5月9日 |
Self-tuning Control of Landing Gear Load |
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| JIA Yu-hong,LIU Ying.Self-tuning Control of Landing Gear Load[J].Acta Aeronautica et Astronautica Sinica,2004,25(3):237-241. |
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| Authors: | JIA Yu-hong LIU Ying |
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| Institution: | Department of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China |
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| Abstract: | The controller is designed by establishing the non-linear model and the ARMAX model of system for the self-tuning of landing gear.The self-tuning control is realized in combination with parameter identification.The simulation results show that the control scheme can effectively improve the absorber capability of landing gear. |
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| Keywords: | landing gear taxing load non-linear model parameter identification self-tuning control |
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