轨道动力学的英文

• dynamics of orbits

• "轨道"英文翻译    track; pathway; rail; runway ...
• "动力学"英文翻译    dynamics; kinetics; power me ...
• "水道动力学" 英文翻译 :    channel dynamics, and
• "国际上泌尿道动力学学会" 英文翻译 :    international society for dynamics of the upper urinary tracts
• "轨道运动力学" 英文翻译 :    orbit mechanics
• "轨道动车组" 英文翻译 :    rail motor set
• "轨道动量" 英文翻译 :    orbital momentum
• "轨道耦合动力学仿真软件" 英文翻译 :    ttisim
• "轨道动量矩矢量" 英文翻译 :    orbital angular momentum vector
• "弹道动力惯性卷筒" 英文翻译 :    ballistically powered inertia reel
• "动力学" 英文翻译 :    dynamics; kinetics; power mechanics
• "力学；动力学；动力；动态" 英文翻译 :    dynamics
• "动力学；力学" 英文翻译 :    dynamics
• "轨道力学" 英文翻译 :    orbital mechanics; track dynamics track mechanics
• "动力的动力学" 英文翻译 :    dynamic
• "monod动力学" 英文翻译 :    monod kinetics
• "Ｓ形动力学" 英文翻译 :    sigmoid kinetics
• "板块动力学" 英文翻译 :    plate dynamics
• "饱和动力学" 英文翻译 :    saturation kinetics
• "爆发动力学" 英文翻译 :    pyrodynamics
• "表观动力学" 英文翻译 :    apparent kinetics
• "表皮动力学" 英文翻译 :    epidermar kinencs
• "冰川动力学" 英文翻译 :    glacier dynamics
• "波动动力学" 英文翻译 :    wave dynamics
• "波动力学" 英文翻译 :    mechanics, wave; wave machanics; wave mechanics; wave mechannics; wave-mechanics

• In order to calculate the orbit of the satellite , we established satellite movement model based on celestial mechanics and spaceflight dynamics
  为满足卫星轨道递推计算需要，根据天体力学、航天动力学理论，建立起二体条件下的卫星轨道动力学模型。
• The orbit simulation program mainly concentrates on orbit calculation . this thesis first introduces the fundamental knowledge of orbit dynamics , including orbit perturbation and spacecraft attitude control
  轨道仿真程序核心部分是轨道计算，本文首先介绍了轨道动力学基础，包括轨道摄动问题，以及飞行器姿态控制等基础知识。
• Optimization of system and mission based on genetic algorithm ( ga ) about geo satellite using mpt has been probed after analysis of orbit dynamics , and building of mathematic model about geo satellite platform and each subsystem
  通过geo卫星轨道动力学分析，建立了卫星总体和各子系统的数学模型。采用遗传算法( ga )对mpt用于geo的ot和nssk进行了系统和任务优化计算。
• Realize the creation of complicated three - dismensional geometric model of space targets by using 3ds data . 3 . based on the track dynamic theory and developed computer software , the system is designed using powerful vc programming language and opengl
  3 .以轨道动力学理论为基础,结合当前成熟的计算机软件技术,采用功能强大的vc编程语言和opengl开发库进行了系统设计,开发了空间目标可视化系统。
• 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。
• In deep space exploration missions , autonomous navigation technology is very important , and in this paper , we do some research into the autonomous navigation schemes of encountering small celestial bodies . it is mainly described as the follows : firstly , by analyzing the orbit characteristics and task requirements in encounter , the simplified orbit dynamic model for the deep space probe is built up , and whether the corresponding model error that meets the demanding of autonomous navigation task is validated
  在深空探测任务中,自主导航技术是十分重要的,本文对交会小行星的自主导航方法进行研究,主要内容包括:首先,分析交会小行星的轨道特性及任务需求,建立简化的深空探测器轨道动力学模型,并验证了简化模型的误差能否满足自主导航任务的需求。
• The research on autonomous navigation and orbital keeping technology of geosynchronous satellites : selecting position vector in the inertia space and longitude , latitude , radial errors in the hill equation as state variables , the precision of orbit determination caused by track dynamic model error , sampling period , and sensor measurement and install error is analyzed
  同步卫星自主导航与轨道保持技术研究：分别选取惯性空间位置矢量和采用hill方程表示的经、纬、向径误差作为状态量，分析轨道动力学模型误差、采样周期以及敏感器测量、安装等误差对定轨精度的影响。
• So combine the item of “ space targets surveillance photoelectricity telescopes arrays system ” , this thesis does research in developing space targets visualization system . the main achievement in this thesis can be summarized as follows : 1 . expatiate e the basic theory of satellite track dynamic , analyse the orbit characteristic of two - body problem and launch window , subastral point calculation , visibility and coverage analysis , two - line element sets
  本文结合“空间目标监视光电望远镜阵系统”课题,进行了空间目标可视化系统的设计和研究,主要作了以下几方面的工作: 1 、阐述了卫星轨道动力学的基本原理,分析了二体轨道特性和发射窗口的基本特性,星下点轨迹计算、可见性和覆盖分析和两行根数。

• 轨道动力学的日语：きどうりきがく