轨道根数的英文

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"轨道根数"怎么读用"轨道根数"造句

英文翻译手机版

elements of an orbit
elements of orbit
orbital elements

"轨道"英文翻译 track; pathway; rail; runway ...
"根数"英文翻译 radical; root
"两行轨道根数" 英文翻译 : tle
"密切轨道根数" 英文翻译 : osculating element
"卫星轨道根数（又称“卫星轨道参数”）" 英文翻译 : orbit elements of satellite
"道根" 英文翻译 : orbital elements
"根数" 英文翻译 : [数学] radical; root
"曹道根" 英文翻译 : cho do geun; cho do-geun
"朴道根" 英文翻译 : park do keun; park do-keun
"发根数" 英文翻译 : number of roots
"平根数" 英文翻译 : mean element
"重根数" 英文翻译 : multiplicity
"贝塞耳根数" 英文翻译 : besselian elements
"不尽根数" 英文翻译 : surd number
"布莱根数" 英文翻译 : bulygen number
"单丝根数" 英文翻译 : number of filaments
"根，根号，根数，根式" 英文翻译 : radical
"根式；根号；根数" 英文翻译 : radical
"交食根数" 英文翻译 : element of eclipse
"庞加莱根数" 英文翻译 : poincare elements
"受摄根数" 英文翻译 : perturbed elements
"瞬时根数" 英文翻译 : instantaneous elements
"吻切根数" 英文翻译 : osculating elements
"正则根数" 英文翻译 : canonical elements
"轨道" 英文翻译 : 1.(供火车、电车等行驶的由条形钢材铺成的路线) track; pathway; rail; runway; circle; railway 地铁轨道 underground railway track; 矿车轨道 tram road; 你将在8号轨道找到你的列车。 you'll find your train at track 8.2.(天体在宇宙间运行的路线) orbit; trajectory 火星轨道 the orbit of mars; 把人造地球卫星送入轨道 put a man-made earth satellite into orbit; 卫星被射入环绕月球的轨道。 the satellite was launched into orbit around the moon.3.(规则; 范围) course; path 偏离轨道 leave the path of righteousness; err from the right path; take a wrong path; 生产已经走上轨道。 production has already been put on the right track.; 轨道变换 [天文学] orbital transfer; 轨道车 motor-trolley; 轨道导弹 orbital missile; 轨道导航仪 orbit navigator; 轨道发射 orbital launching; 轨道方向 [航空] orbital direction; 轨道飞行器 orbiter; 轨道敷设 track laying; 轨道火箭 orital rocket; 轨道计算 orbit(al) determination; 轨道交角 inclination of orbit; 轨道空间 orbit space; trajectory space; 轨道空间站 [天文学] orbital space station; 轨道力学 orbital mechanics; 轨道偏移 orbit displacement; 轨道平面 [力学] orbital plane; 轨道倾角 orbit inclination angle;轨道曲线 [航空] orbital curve; 轨道速度 orbital velocity; 轨道卫星 orbiter; orbiting satellite; 轨道修正 orbit trimming; 轨道运动 orbital motion; 轨道中心 orbit centre

例句与用法

Autonomous relative orbit determination for satellite formation flying on basis of orbit element differences
基于轨道根数差的卫星编队自主定轨研究
The secular influence of solar mass - loss on the orbital elements of meteor steams is examined by using the method of celestial mechanics of variable mass in this paper
摘要将作者在变质量天体力学所得理论结果应用于太阳质量损失对流星群轨道根数变化的长期效应上。
Firstly , this paper presents the coordinates and time system for discribing satellite motion , and then gives the models of orbit and attitude and satellite relative motion , considered the j2 perturbation
本文首先给出描述卫星运行所需的时间系统和坐标系，然后建立卫星轨道、姿态动力学模型和基于轨道根数的卫星编队飞行相对运动方程，并考虑j2项摄动的影响。
The numerical computation for the secular variable of the semi - major axis , solar distance at perihelion , orbital periods and longitude of perihelion has been made for fifteen meteor streams by using the solution of gylden - meshcherckii equations
利用g - m型变质量天体轨道根数变化方程的一阶和二阶解对15个流星群轨道半长轴、近日点距离、轨道周期和近日点经度因太阳质量损失造成的每世纪的长期改变效应做了数值计算，并得出计算结果。
By analyzing the inter - satellite measurement net of walker constellation at some time in geometry and numeric , the correction of system error and random error caused by the change of orbit elements using different type of estimation of inter - satellite measurement net was provided quantitatively
并通过对walker星座某一时刻的星间观测网进行几何分析和数值分析,定量给出了利用不同类型的星间观测网对轨道根数变化引起的系统误差和随机误差的修正情况。
Followings are the main study in this paper . 1 ) based on building the condition function of orbit determination of satellite - to - satellite tracking , the coefficient matrix of its normal function was studied . and the relativity of satellite ’ s corresponding orbit elements was analyzed in different cases
本文的主要研究工作如下: 1 )在建立星-星跟踪定轨条件方程的基础上,对其法方程的系数矩阵进行研究,分析了在不同情况下,卫星对应的轨道根数的相关性。
And then , according to the kind of satellite and the requirements for geodetic and astrometric study and the geometry of gnss ( gps , galileo ) satellite to track the space vlbi satellite , the six keplerian elements of chinese space vlbi satellite ( test - svlbi ) are selected and determined
根据卫星轨道的分类、大地测量和天体测量对空间vlbi卫星的要求,以及gnss ( gps和galileo )卫星对空间vlbi卫星跟踪观测的几何条件而设计了我国空间vlbi卫星的六个轨道根数。
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。
Our results show that , during the evolution of a binary system , the system widens as it loses mass , and the orbital period increase , while orbital eccentricity remains nearly constant , which can explain the distribution regulation of orbital elements of normal g - k giant and barium stars and the distribution character of the heavy - element abundances of barium stars
计算结果表明，随着星风吸积过程的进行，在星风质量损失阶段系统轨道半长轴将增大，导致轨道周期增大，而偏心率变化不大，由此可以解释普通红巨星双星系统和钡星系统的轨道根数的分布规律和变化情况以及钡星重元素丰度分布特征。
Then , the chaser ' s two orbit roots are selected as variable and visualizing the simulation by contour plot . this part of research draws the conclusion the same as the first part when the target ' s orbit is circular orbit , while the selected two variable can be wildly changed if the target ' s orbit is elliptical orbit . next , wait time before orbit maneuver is simulated
其次,利用可视化的等值线图研究了追踪器轨道两个参数为变量的情况下大范围轨道机动问题,分析表明对圆轨道目标器交会机动时,追踪器轨道根数不宜与目标器轨道根数相差过大,而对椭圆轨道目标器交会机动时,追踪器轨道根数可选范围较大,机动策略和方法富于弹性。