| 直升机飞行参数综合分析系统的设计与实现 |
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| 引用本文： | 叶飞,彭秀云,王立国,肖阳.直升机飞行参数综合分析系统的设计与实现[J].长沙航空职业技术学院学报,2010,10(2):34-38. |
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| 作者姓名： | 叶飞 彭秀云 王立国 肖阳 |
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| 作者单位： | 总参陆航部驻株洲地区军事代表室,湖南,株洲,412002;总参陆航研究所机体与发动机室,北京,101121 |
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| 摘 要： | 本文的研究目的是实现直升机飞行参数的综合分析,建立了数据采集装置、飞行参数维护子系统、飞行参数信号处理与分析子系统、智能故障诊断子系统、虚拟飞行再现与评估子系统五个部分。阐述了各个子系统的设计思路和方法,系统的设计和实现对于直升机飞参记录系统校验维护、直升机技术状态监控、飞行质量评估和飞行安全及事故分析具有重要的意义。
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| 关 键 词： | 直升机 飞行参数 综合分析 状态监控 |
Design and Realization about Synthesis Analysis System for the Helicopter Flight Parameter |
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| YE Fei,PENG Xiuyun,Wang Liguo,XIAO Yang.Design and Realization about Synthesis Analysis System for the Helicopter Flight Parameter[J].JOurnal of Changsha Aeronautical Vocational and Technical College,2010,10(2):34-38. |
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| Authors: | YE Fei PENG Xiuyun Wang Liguo XIAO Yang |
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| Institution: | 1、Military Representatives＇ Office in Zhuzhou District of Air and Land Branch of the Headquarters of the General Staff,Zhuzhou Hunan 412002;2、The Body and Engine Laboratary of the Air and Land Research Institute of the Headquarters of the General Staff,BeiJing 101121) |
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| Abstract: | The purpose of the paper is to realize synthesis analysis for the helicopter flight parameter.It designs data collection equipment,flight parameter maintenance subsystem,disposal and analyssis subsystem for flight parameter signal,intelligent obstacle diagnosis subsystem and virtual flight emersion and evaluation subsystem,and expatiates the design idea and method for each subsystem.The design and realization of the system has an important meaning for the verification and and maintenance of the helicopter f... |
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| Keywords: | helicopter flight parameter synthesis analysis status monitor |
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