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飞机系统的英文

  • aircraft system

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  • 例句与用法
  • Stress - strength interference model of structure reliability is introduced to analyze human reliability . the decrease speed of strength with time is studied by the human stress - strength interference model , and its probability density function is derived . similar to engineering reliability analysis method , ucav system reliability diagram and fault tree are presented , fmeca is also performed
    论文的第二部分研究无人作战飞机系统的可靠性分析,在对人的差错的原因深入分析的基础上,建立了人的通用差错模型,借鉴结构可靠性分析方法,建立了人的可靠性的应力强度模型,推导了强度随时间下降速率的概率分布;运用工程可靠性分析方法,建立了无人作战飞机系统的可靠性框图、故障树,并且做了人的差错的故障模式影响分析。
  • The total auto symbol recognition disposition method proposed in this paper can deal with the problem which converts papery of aircraft theory graphics or system graphics into vectorgraphs which can lose some useful information . furthermore , the display technique with multi - level buffer not only resolves the problem of high - speed for aircraft theory graphics or system graphics in cbt , but also ensures scrolling and zooming in / out smoothly and avoids the flashing phenomenon efficiently
    目前纸质的飞机系统图、原理图矢量化方法用基本的矢量图元按其位置来再现原始图,从而导致矢量后图中各符号整体信息丢失问题,该文提出的自动符号识别方法可有效地解决该问题,此外改进多级缓冲显示技术不但可有效地解决cbt中系统图、飞机原理图的快速显示,而且也保证图形可连续光滑滚动和消除放缩拖动时屏幕闪烁现象。
  • In the first part , human - machine interface design of ucav ( unmanned combat air vehicle ) is studied . the design criterion of display , controller and working environment for human in ucav system is presented . in the second part , based on the analysis of human error cause , human generic error model is presented
    论文的第一部分研究无人作战飞机系统的人机界面设计,论文给出了无人作战飞机系统的功能框图,根据无人机的任务剖面,综合功效学的研究成果,给出了无人机系统的显示装置、控制装置、工作环境和操作人员的组织情况等的设计准则。
  • The nonlinear decoupling method applied on full , hi - fidelity aircraft analysis model was unprecedented , many technique , such as disassemble - design , assemble - apply , multi - grade decoupling , were used so that the nonlinear decoupling method can be used on such a complex model . the successful design of a roll angle and overload decoupling controller show that the nonlinear decoupling is a feasible method for engineering application
    非线性解耦方法在高真实度的完整飞机系统分析模型上的应用在国内尚属,文中采用分解设计、组合应用、多级解耦控制结构等方法,解决了非线性解耦方法难于应用于复杂系统的问题,成功地设计了滚转角及过载解耦控制器,达到了较好的控制效果,为工程设计提供了新的途径。
  • 更多例句:  1  2
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Last modified time:Thu, 14 Aug 2025 00:29:56 GMT

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