| 主动控制起落架滑行性能分析 |
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| 引用本文： | 贾玉红,何庆芝,杨国柱.主动控制起落架滑行性能分析[J].航空学报,1999,20(6):545-548. |
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| 作者姓名： | 贾玉红 何庆芝 杨国柱 |
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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 |
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| 摘 要： | 建立了主动控制起落架的非线性振动模型，并通过建立系统的状态方程和合理的目标函数，使系统的综合性能达到最优。通过数值模拟计算，对主动控制起落架和被动起落架的滑行性能进行了比较。
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| 关 键 词： | 起落架 主动控制 非线性振动 滑行性能 |
TAXIING PERFORMANCE ANALYSIS OF ACTIVE CONTROL OF LANDING GEAR |
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| JIA Yu-hong,HE Qing-zhi,YANG Guo-zhu.TAXIING PERFORMANCE ANALYSIS OF ACTIVE CONTROL OF LANDING GEAR[J].Acta Aeronautica et Astronautica Sinica,1999,20(6):545-548. |
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| Authors: | JIA Yu-hong HE Qing-zhi YANG Guo-zhu |
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| Institution: | Dept. of Flight Vihicle Design and Applied Mechanics,Beijing Univ. of Aero. and Astro., Beijing 100083, China |
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| Abstract: | A non linear model of active control of the landing gear has been established. According to the state equations and a reasonable objective function, the comprehensive performance of landing gear is optimized. By numerical simulation, the taxiing performance of an active control system landing gear and that of a passive system landing gear are compared. |
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| Keywords: | landing gear active control non linear vibration taxiing performance |
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