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flight characteristics中文是什么意思

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用"flight characteristics"造句"flight characteristics"怎么读"flight characteristics" in a sentence

中文翻译手机手机版

  • 飞行特性

例句与用法

  • Influence of spraying distance on flight characteristics and deformation of particle
    喷涂距离对粒子飞行特征及变形程度的影响
  • Analyzing to a stand off missile ' s flight characteristics , the as missile trajectory simulation is completed
    在分析了典型防区外导弹飞行特点的基础上,进行空地导弹弹道仿真。
  • The composite grips extend bearing life , while working with the innovative two - stage dampening to give the n9 incredible flight characteristics
    综合枪柄轴承延长寿命,同时与创意两阶段调高给n9不可思议的飞行特性
  • Not only does the photo show a flying saucer , but the flight characteristics described by the witness defy conventional aerial motion because the object was moving rapidly , stopped , hovered , and then sped off
    不仅图片表现出飞碟,但飞行特性描述的证人藐视常规空中议案,是因为物体移动快,停,盘旋,然后迅速赶过
  • In order to study the flight characteristics and control rules in taking off and landing period better to promote flight safety of uav in this stage , we started the study of take off and landing simulation system research of uav based on a certain type of uav
    为更好地研究无人机在起飞、着陆阶段的飞行特性,控制规律,以保证无人机在这一阶段的飞行安全,我们以某型无人机为对象进行无人机的起飞、着陆仿真系统研究。
  • Through calculating and analyzing basic performance , the flight characteristic of the towed system is researched . stability and control issue of carrier rocket is discussed primarily . the net result of the thesis will prove the feasibility of the scheme of towed launch
    论文通过牵引系统基本性能的计算和分析,完成牵引飞行特性的研究,同时对运载器的稳定性和控制问题进行初步的探讨,最终结果将验证牵引发射方案的可行性。
  • The flight characteristics of high altitude long endurance uav are analyzed , several typical kinds of aeronautical weather are ingathered , and the vertical distributing model of large scale windfield is established , traditional numerical simulation methods of atmosphere environment are summarized . 2
    分析了高空长航时无人机的飞行特点,统计了几种的典型航空气象特征,并提出大尺度风场的垂直分层型,最后总结了大气风场的常用数值模拟方法; 2
  • 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。
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