离轨的英文

• aberrance

• "电离轨道" 英文翻译 :    ionization path; ionization track
• "离轨速度" 英文翻译 :    take-off velocity
• "偏离轨道" 英文翻译 :    side track; veer off course; deviate from course
• "脱离轨道" 英文翻译 :    de orbit; deorbit; escape orbit; off road; orbit exit
• "远离轨道" 英文翻译 :    far-out orbit
• "偏离轨道误差" 英文翻译 :    off-track error
• "脱离轨道运行" 英文翻译 :    deorbit
• "脱离轨道装置" 英文翻译 :    jump-down device
• "双曲线脱离轨迹弧" 英文翻译 :    hyperbolic arc; hyperbolic escape arc
• "脱离轨道的卫星" 英文翻译 :    jump-down satellite
• "分离轨道回旋加速器" 英文翻译 :    separated orbit cyclotron; seperated-orbits cyclotron
• "航天器脱离轨道通知" 英文翻译 :    spacecraft de-orbit notification
• "脱离轨道火箭发动机" 英文翻译 :    de-orbit rocket
• "脱离轨道用的制动发动机" 英文翻译 :    deorbit engine
• "脱离轨道制动火箭发动机" 英文翻译 :    de-orbit-retro rocket
• "分离轨道强聚焦回旋加速器" 英文翻译 :    strong-focusing cyclotron with separated orbits
• "脱离轨道用的制动火箭发动机" 英文翻译 :    deorbit retrorocket engine
• "离光束轴散射" 英文翻译 :    off beam axis scattering
• "离国服务工作人员" 英文翻译 :    expatriate staff
• "离光标点最近的快速选取位置" 英文翻译 :    place quick pick near cursor
• "离国福利" 英文翻译 :    expatriate benefits
• "离管型薄壁组织" 英文翻译 :    apotracheal parenchyma
• "离国津贴" 英文翻译 :    expatriation allowance
• "离管菌属" 英文翻译 :    fistulina
• "离国庆节很近了" 英文翻译 :    it'll soon be national day
• "离管带状薄壁组织" 英文翻译 :    apotracheal banded parenchya; apotracheal banded parenchyma

• I don ' t think we have to worry so much about him straying that far
  我想我们不必担心他会离轨那么远
• I don ' t think we have to worry so much about him straying that far
  我想我们不必担心他会离轨那么远
• All of this is already mapped out , and she knows just how far to go without knocking herself completely off course
  这所有的一切是已经被安排，而且她就是知道分寸不会让她自己完全地震离轨道。
• However , einstein reasoned that it should take longer for the planets farthest from the sun to find out what happened , so the closet planets should fly out of orbit first
  可是，爱因斯坦以详细的理由说明离太阳越远的行星会越迟知道太阳消失了，所以较近的行星会先飞离轨道。
• The principle of how to supply energy for system has also been studied . secondly , the orbiting satellites are affected by several perturbations . we put the main emphasis on the influence of the perturbations of the atmosphere drag and the earth ’ s eccentricity on the six orbital factors and the simulation ’ s accuracy
  其次,卫星在轨运行时将受到各种干扰力的影响,因此在研究精确地磁场模型电动力缆绳离轨系统的动力学特性的基础上,着重研究了大气阻力摄动和地球非球形摄动对卫星离轨过程中各轨道参数的影响。
• Finally , by modifying the configuration parameters of tether ’ s length and radius , we have analyzed the influence of the tether configuration . the results of simulations show that if shorten the tether ’ s length , the duration of de - orbiting will show a marked increase , and if increase the tether ’ s radius , the duration of de - orbiting will show a marked decrease
  最后,改变了电动力缆绳的长度和直径大小,分析了电动力缆绳参数变化对离轨时间的影响,仿真结果表明,缩短缆绳长度离轨时间明显增加,而增大缆绳的直径,离轨时间将显著减少。
• In this application , the lorentz force generated by the interaction between the current in the wire and the geomagnetic field produces an electro - dynamic drag leading to a fast orbital decay . in this paper , we make an intensive study of the process of de - orbiting using electro - dynamic tether system . the concrete work includes : firstly , i have studied the basic principle of how to generate the electro - dynamic drag , modeled via accuracy geomagnetism , made a concrete analysis of the de - orbiting duration , the magnitude and direction of electro - dynamic drag under the action of the dipole and accurate geomagnetic models , set up a counterbalance between electro - dynamic torque and gravity gradient torque , emulate the de - orbiting process of spacecraft , and compared the change of six orbital factors and the de - orbiting duration under the action of the dipole and accurate geomagnetic models
  本文对基于电动力缆绳的航天器离轨过程进行了深入研究,具体工作如下:首先,本文研究了电动力缆绳产生电动力拉力的基本原理,建立了精确地磁场模型;分别在偶极子模型和精确地磁场模型作用下,对电动力拉力的大小、方向、离轨时间及电动力缆绳倾角的大小进行了计算分析;建立了电动力力矩与缆绳系统重力梯度力矩的平衡关系;分析了电动力力矩为系统提供能量的原理;最后分别在偶极子地磁场模型和精确地磁场模型作用下,对受电动力缆绳作用的航天器的离轨过程进行仿真,分析了在不同精度地磁场模型下,航天器离轨过程中各轨道参数的变化情况,并比较了不同模型对离轨时间的影响。

• 离轨的韩语：[동사] (1)【약칭】〈우주항공〉 궤도를 벗어나다[이탈하다]. [‘脱tuō离轨道’의 준말] ↔[入rù轨] (2)【비유】 바른길을 이탈하다. 상궤(常軌)를 벗어나다.