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飞机滑行中差动刹车性能的仿真测试
引用本文:周涛.飞机滑行中差动刹车性能的仿真测试[J].航空计测技术,2011(6):7-10.
作者姓名:周涛
作者单位:上海飞机设计研究院,上海200235
摘    要:转弯能力是体现飞机控制能力的一项重要指标,有多种方式实现此功能。对于突发事件,主轮刹车是对飞机转弯能力的重要补充。本文针对飞机着陆滑跑状态,综合考虑在运动中飞机所受的多种干扰,对飞机状态进行模拟测试,分析飞机在跑道上的受力,设定一个利用主轮刹车系统进行辅助转弯控制的方案,完善飞机主起落架的刹车特性分析工作。

关 键 词:应急状态  飞机转向  主轮刹车系统

Performance Simulation of Aircraft Asymmetry Brake
ZHOU Tao.Performance Simulation of Aircraft Asymmetry Brake[J].Aviation Metrology & Measurement Technology,2011(6):7-10.
Authors:ZHOU Tao
Institution:ZHOU Tao(Shanghai Aircraft Design and Research Institute,Shanghai 200235,China)
Abstract:The capability of airplane control on the ground is considered very important.There are some methods to accomplish this function.In the special landing situation of aircraft,the capability of brake should be considered.Combined with civil airplane are based on the characteristics of the airframe ground force,the model of airplane during ground roll and taxi is established.A scheme of main wheel brake system for trajectory bias rectification control is assumed.Analysis gives the characteristic of main wheel brake system in condition of ground turning control.
Keywords:emergency state  aircraft ground operation  main landing gear brake system
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