机动的的英文

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英文翻译
造句

automobile
automotive
flexible
maneuverable
mechanically driven
mechanically propelled
motor drawn
motor-driven
power operated
power-actuated
power-drawn
powerdriven
poweroperated
power-propelled
powered
self-propelled
self-propelling

机动 motor-driven; motorized flex ...
的 4次方是 The fourth power of 2 i ...
半机动的 semi mobile; semimobile; semimechanical
非机动的 non-maneuverable; non-powered; nonpropelled
高度机动的 highly maneuverable
机动的打法 moving play
机动的来源 mobile sources
机动的；发动机驱动的 engine-driven
自动的，机动的；汽车的 automotive
不机动的战术 standing play
机动的地面视察 mobile ground inspection
可机动的航天器 maneuverable spacecraft
灵活多变的,机动的 mobile
实施机动的集团 mass maneuver
四轮驱动的机动车 four-wheel drive motor vehicle
发动机动的同步发电机 engine alternator
灵活机动的战略战术 flexible strategy and tactics
骑在马背上的，机动的，架好的 mounted
机动 1.(利用机器开动的) motor-driven; motorized2.(权宜; 灵活) flexible; expedient; mobile; manoeuvrable 机动处置 deal with sth. flexibly; 灵活机动的战略战术 flexible strategy and tactics3.(准备灵活运用的) keep in reserve; for emergency use 机动力量 reserve force; 机动时间 time kept in reserve; 机动资金 a fund kept in reserve; 留百分之二十作机动开支 keep back 20% for extras; 机动保险 motor vehicle insurance; 机动财力 stand-by financial resources; 机动车辆 motor-driven vehicle; motor vehicle; mechanically-propelled vehicle; motor-coach; rolling-stock; 机动粮 grain reserve for emergency use; 机动炮 mobile artillery; 机动时间 cutting time; machine time; 机动税 sliding duties; 机动自行车 moped; 机动装置 tracker action
滑水(以机动船拖动的乘浪滑行运动) wake surfing
可机动的再入大气层运输火箭系统 maneuverable re-entry ferry system
动的 kinetic; motional; motive; moving
摆动的；振动的 oscillating
被动的，从动的 driven
流动的, 变动的 fluxionary

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例句与用法

According to different anticipative collisional time and maneuver occasion , author established two maneuver mathematic model , and gave the principle and occasion executing the de - orbit and de - contrail maneuver procedure . forth , author complied the orbit early warning and collision avoidance software
根据不同的预期碰撞时刻和采取轨道机动的时机,建立了两种规避策略数学模型,并据此分析提出了两种规避方法高度分离法和轨迹分离法的原则和时机。
Then similar human intelligent control method is selected to control movement of rolling base . in order to overcome modeling and control difficulty of flexible multibody structure , decentralized modeling method based on structural identification and decentralized predictive control is studied
根据这个控制策略，分别系统地研究了中心刚体机动的仿人智能控制方法和柔性多体结构的分散预测控制方法，设计了具有组织级、协调级和执行级的组合结构振动主动控制器。
With the development of material technology , information technology , automation control technology , aeronautics and astronautics technology , the modern flight vehicles are required of high velocity , light structure , great flexibility and super maneuverability , which lead to the serious aeroelastic effects such as aeroservoelasticity , the coupling among the aerodynamics , structure , and control system
随着材料技术、信息技术、控制技术以及航空航天技术本身的飞速发展，飞行器开始向高速度、轻结构、大柔性、超机动的方向发展，气动弹性效应更加严重，从而引发了气动、结构、控制系统相互耦合的气动伺服弹性力学问题。
The basis of dynamics and simulation includes the iterative flyout angle algorithm to the solutions to lambert problem and battin ' s universal conic section state extrapolate method . then spacecraft ' s orbit roots , maneuver impulse and maneuver time are discussed as the following four part : first of all , the chaser ' s one orbit roots is selected as a variable to simulate its influence to the large scale orbital maneuver . the research reveals fact that the orbit roots both of chaser and target should be close to each other to achieve better maneuver and rendezvous " ability , moreover , the best orbit maneuver and rendezvous occurs when both chaser and target ' s initial phase angle are equal
为了研究了交会机动中追踪器和目标器的轨道根数、机动时限和机动能耗等因素对交会机动的影响,仿真和分析分为以下四个部分:首先,研究了追踪器轨道单个参数为变量情况下两航天器大范围交会机动问题,研究表明,追踪器的变化参量与目标器相应的参量在接近的情况下可以获得良好的交会机动特性,而对于两航天器轨道共面的情况下,初始相位角相等时则获得最佳的机动效果。
The second part studies optimal pure proportional navigation ( ppn ) , with time - dependent gain of navigation to maneuvering target based on proportional navigation theory . optimal gain of navigation is constant for ppn without maneuvering ; based on this , solution of time - dependent gain of navigation is given by iteration approach , and the time required for capture is given , the times of iteration is decided by comparing this time with the iteration step
对目标机动的追逃问题,考虑导航增益可为任意实数,且随时间和初始条件改变,这一思想是建立在目标非机动的纯比例导引制导规律,最佳导航增益为常数的基础之上,利用迭代的方法,给出了时变的导航增益的求解方法,并给出了实现捕获所需的时间,用此时间与迭代步长进行比较,判定迭代次数。
Because formation satellite ' s relative position is very close and the geometry can change easily , based on the relative motion of satellites , the initial phase bias could be quickly resolved simulation solution indicates that phase bias can be determined quickly and the relative states accuracy should be improved by using initial phase bias
由于编队卫星相对距离近，相对构型容易改变，因此采用卫星相对机动的方式进行整周模糊度的快速初始化。仿真结果表明，基于卫星机动，整周模糊度可很快初始化。利用初始化的整周模糊度，相对状态的解算精度会大大提高。
It ' s presented that the research of shortwave datacomms modem in the communication equipment test , which is developed to meet the demand of efficient and reliable shortwave little information point to point datacomms by routine communication device in maneuver situation
本文所做的调制解调器的研究是在短波数据通信中提高抗干扰能力的一个试验项目，重点解决军事通信在应急机动的条件下，使用简单常规的通信设备，利用短波信道，有效可靠地进行小信息量的点对点数据传输。
In addition , the principle of component synthesis vibration suppressing ( csvs ) method is also briefly introduced and summarized to several lemmas , which can suppress flexible vibration by utilizing the character of vibration system itself and has the characters of simple , multiform , easy to apply and so on
另外,为了将分力合成方法应用于挠性系统的振动抑制,简要地介绍了分力合成方法的一些基本概念及原理。针对采用推力器作为执行机构的挠性航天器姿态机动的振动抑制问题,提出了将分力合成振动抑制( csvs )方法和基于分布压电元件( pzt )的主动振动抑制技术相结合的一种复合主动控制方法。
Mature companies with the expertise and strive to perfect attitude , a new r & d printing equipment , its cost - effective , won widespread praise , but also rely on sophisticated technologies and the concept of sustainable development formed a special rapid mobility aftermarket team , for your sense of lifting production
公司凭借成熟的专业技术和力求完美的态度，研发了新颖的网印设备，其高性价比赢得了客户的广泛好评，同时公司还依托娴熟的技术和永续经营的理念特组建了一支快速机动的售后队伍，为您的生产解除忧患。
About the large deformation description , a multi - floating coordinate system is adopted . it can effectively reduce the error of discretization . this paper deals with the design of restrained variable structure control in the way of phase plane analyse , which is concise and avoids complex mathematical descriptions . a new method is promoted for flexible spacecraft control by describing flexible spacecraft dynamics equations as t - s fuzzy model and designing a pdc fuzzy controller
将挠性航天器姿态动力学方程描述为t - s模糊模型为挠性航天器控制提供了新思路;仿真结果表明,基于t - s模型的pdc模糊控制器能满足挠性航天器大角度姿态机动的精度要求,并能有效抑制帆板振动,具有一定的智能性。