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大气阻力的英文

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"大气阻力"怎么读用"大气阻力"造句

英文翻译手机手机版

  • atmospheric drag
  • atmospheric resistance
  • atmospherical drag

例句与用法

  • The effect caused by the atmospheric drag is investigated also
    文中还研究了大气阻力对卫星编队飞行的影响。
  • Atmospherical drag perturbation
    大气阻力摄动
  • Atmospheric drag acceleration
    大气阻力减速
  • The algorithm and related influencing factors , such as gravitational model , atmospheric drag , sample intervals and filter parameters , are deeply analyzed , and some important conclusions are deduced
    对定轨算法及其主要影响因素,如地球引力场、大气阻力、采样间隔和滤波参数等进行了深入分析,并得出一些重要结论。
  • For example , it can be used to drag make - up and solar pressure cancellation of low orbit spacecraft , formation flying and precise positioning of small satellite , repos
    同时, mpt也可用于低轨道( 300 500km )航天器的大气阻力补偿,星际航行航天器的主推进,以及星座和小型卫星的编队飞行和精确定位等,具有广阔的应用前景。
  • Unlike comet and asteroid orbital elements which can be reliably used for many months , satellite orbits are constantly changing due to both orbital maneuvering by the satellite and the effects of atmospheric drag
    小行星和彗星的轨道计算数据可以使用数月,但是人造卫星不行,因为它们的轨道会随时被人造卫星自己或者大气阻力所修正。
  • Much attention is paid to the effect of perturbations on satellite formation flying and how to decrease the effect , which are studied with the earth oblateness and atmospheric drag considered
    摄动因素对卫星编队飞行的影响以及如何尽量减小摄动影响是应用中非常关心的问题,本文考虑地球扁率和大气阻力两种摄动因素,对此进行了研究。
  • Taking account of the perturbation of the earth ’ s shape , the gravitation of the sun and the moon , the radiation pressure from the sun light and atmosphere drag , a precise orbital dynamic model of spacecraft is established in the equatorial geocentric inertial coordinate system ( j2000 )
    考虑了地球形状摄动、日-月引力摄动、太阳辐射压力和大气阻力因素对飞行器的影响,在地心赤道惯性坐标系下建立了精确的轨道动力学模型。
  • 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。
  • The main work done in the paper is as follows : 1 . satellite attitude dynamics modeling study : for the earth - oriented three - axis stabilized satellite , a precise attitude dynamics model is established , considering the influence of the environmental disturbance , such as the gravity , the sun radiation , the earth magnetic field and the atmospheric resistance
    本文的主要研究工作如下: ( 1 )卫星姿态动力学建模研究:针对对地定向三轴稳定卫星,考虑了重力梯度、太阳辐射、大气阻力、地球磁场等环境因素对卫星的影响,建立了较精确的卫星姿态动力学模型,同时又建立了四元素描述的姿态运动学方程。
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