飞行控制计算机的英文

• flight-control computer

• "飞行"英文翻译    flight; flying; aviate; voya ...
• "控制计算机"英文翻译    control computer
• "飞行控制计算器" 英文翻译 :    flight control computer
• "主飞行控制计算器" 英文翻译 :    flight control primary computer
• "控制计算机" 英文翻译 :    control computer; control coputer
• "保密控制计算机" 英文翻译 :    security control processor
• "波束控制计算机" 英文翻译 :    beam controlling computer
• "车辆控制计算机" 英文翻译 :    wagon control computer
• "程序控制计算机" 英文翻译 :    pcc; program computer; program controlled computer; program controlled device; programmable computer; programmed computer; programmed machine; self-programming computer; sequence controlled computer; sequence-controlled computer; sequential control counter
• "次序控制计算机" 英文翻译 :    sequence-controlled computer
• "点火控制计算机" 英文翻译 :    spark-control computer; spark-lug gap
• "分散控制计算机" 英文翻译 :    decentralized computer
• "工业控制计算机" 英文翻译 :    industrial control computer; process computer
• "管理控制计算机" 英文翻译 :    supervisory control computer
• "过程控制计算机" 英文翻译 :    proce computer; proce control computer; process computer; process control computer; processcomputer
• "和序控制计算机" 英文翻译 :    program-controlled computer
• "呼叫控制计算机" 英文翻译 :    call control computer
• "混合控制计算机" 英文翻译 :    hybrid control computer
• "火花控制计算机" 英文翻译 :    spark control computer
• "火力控制计算机" 英文翻译 :    fire control computer
• "货物控制计算机" 英文翻译 :    freight control computer
• "机床控制计算机" 英文翻译 :    machine tool control computer
• "监督控制计算机" 英文翻译 :    scc; supervisory control computer
• "交换控制计算机" 英文翻译 :    switch-hook flash
• "控制计算机子系统" 英文翻译 :    control computer subsystem

• Meanwhile the designed parameter can be loaded into the real - time simulation platform and joined hi the simulation of the whole flight control system , hi addition , all the flight data from the simulation will be shown hi real time and analyzed hi the design platform
  该系统可以对常规pid控制方式下的飞行控制系统进行可视化参数设计、动态调整参数，并且可以将设计好的系统参数装载入实时仿真平台，并作为虚拟飞行控制计算机参与整个飞行控制系统的实时仿真。
• The modern unmanned helicopter flight control system is generally composed of the flight control computer , the servo driving mechanism , the sensor , and the ground monitor control system etc . in this thesis the research to the helicopter flight characteristics was conducted at first , and its flight dynamic model was preliminary discussed , especially the mathematic model under hung - stop condition was formulated and the algorithm of the controller was designed in detail
  现代无人直升机飞行控制系统一般由飞行控制计算机、伺服驱动机构、传感器、地面监测控制等分系统组成。本文首先对直升机的飞行特性进行了研究,并且对飞行动力数学模型做了初步探讨,尤其对在悬停状态下的数学模型做了较为详尽的公式推导和控制器的算法设计。
• Most countries in the world attach importance to the use of long - time uav ( unmanned aerial vehicle ) in the military . the kernel question of long - time uav is how to improve the reliability of flight control computer . the research of how to improve the reliability of flight control computer has became more and more important today
  长航时无人机的重要性尤其在军事上已经得到国内外的高度重视，其核心飞行控制计算机(以下简称“飞控计算机” )的可靠性问题变的日益突出，对其容错研究成为当今的热点。