- 更多网络例句与轨道倾角相关的网络例句 [注：此内容来源于网络，仅供参考]
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The absolute coding model360°angle sensor is us ed for inducing the angles and positions of the track type sphere welding machin e.Knowing the distances from two end points of the track to the weld-groove w e calculated,mathematics formulas of the distance of the any position of track to weld-groove.
采用了一种绝对编码式360°倾角传感器作为轨道式球罐焊机的角度位置传感器，在已知轨道两端点至焊接坡口横向距离的前提下，进行了整个轨道任意位置与焊接坡口间横向距离的数学公式推导。
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Design variables include the artificial satellite number, orbit inclination angle, geographic longitude of intersection of two constellations, and every constellation is hit by the 1st artificial satellite phase angle.
提出IGSO星座的优化设计方法：以一种双"8"字形、共轨道面的IGSO星座构型为例进行星座设计，设计变量包括卫星数目、轨道倾角、2个星座的交点地理经度，每个星座中第1颗卫星的相位角。
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The results show that high inclination circular high orbit(150 km or 200 km) has better performance,with its orbit lasting more than one yea...
大量的仿真计算表明，高倾角、圆轨道的中低轨(150 km或200 km)绕月飞行器具有相对稳定的轨道演化特征，在不进行任何调整的情况下，其轨道持续运行时间超过1 a。
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The orbit of the equatorial satellite is designed with perigee at 550km, apogee at 60 000km, and the inclination of 28.5°; the orbit of the polar satellite is designed with perigee at 700km, apogee at 40 000km, and the inclination of 90°.
近地赤道区卫星的轨道是：近地点550km左右，远地点60000km左右，倾角约28.5°；近地极区卫星的轨道是：近地点700km，远地点40000km，倾角约90。
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Using inclination vector as a non-singular orbital element, engineering oriented mathematical models for inclination control of geosta- tionary orbit are established,and unified optimal strategies for inclination control both in north-south station aquisition and north-south station keeping derived.
本文以倾角矢量作为无奇点轨道要素，建立静止卫星轨道倾角控制的工程实用数学模型，进而导出南北定点捕获和南北位置保持两种情况下统一的倾角控制燃料最优策略。
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In this paper, the impacts of 4 types of LEO orbit parameters —argument of latitude, right ascension of ascending node, orbit height and inclination—on the distribution and number.
分析了对于单颗LEO卫星，掩星事件的分布和数量随着LEO 轨道参数包括轨道升交角距、升交点赤经、轨道高度和倾角而变化的规律，并得出了相应结论。
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The line that passes through the center of the Earth linking the perigee and apogee, known as the line of apsides, itself rotates in the orbital plane at a speed that depends on the geometry of the elliptical orbit and the inclination of the orbital plane to the equator.
经过地球中心，连接近地点和远地点的线称为apside线，卫星在轨道平面上以某个速度旋转，这个旋转速度根据椭圆轨道以及轨道平面到赤道的倾角的几何学来计算。
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Since geostationary satellite s orbit inclination is equal to zero approximately,it will result in the ambiguity of satellite s orbit ascending node and the singularity of the normal matrix in the process of fitting.
针对静止轨道卫星轨道倾角近似为0，致使卫星轨道的升交点定义模糊，在数据拟合过程中会导致法矩阵奇异的问题，提出对卫星轨道进行轨道倾角变换拟合广播星历参数的方法，并获得较高的拟合精度。
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Because of the secular perturbation variations of the ascending node right ascension, the argument of perigee and the mean angle caused by the initial deviations of the semi-major axis, the inclination and the eccentricity are linear time-variant, then the active biases of the semi-major axis, the inclination and the eccentricity can realized the self-stabilization design of the elliptical orbit satellite constellation, and so the configuration stability will be improved.
通过初始偏差对椭圆轨道卫星的长期影响分析可知，轨道半长轴、倾角和偏心率的初始偏差对升交点赤经、近地点幅角和平近点角的长期摄动变化是线性的，因此通过主动偏置轨道半长轴、偏心率和倾角能够实现椭圆轨道星座构型的自稳定设计，从而提高其构型稳定性。
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The following conclusions are drawn. 1 The orbit parameters that have relatively greater influence on the number and latitudinal distribution of annual occultation events are orbit inclination, orbit height, Right Ascension of Ascending Node and Argument of Perigee in turn. All four parameters have little impact on the longitudinal distribution of annual occultation events. 2 The orbit inclination of Transmitting Satellite and Receiving Satellite impacts both LEO－LEO occultation events number and their latitudinal distribution most. The number of occultation events reaches the maximum as the sum of the two inclination angles nears 180 degrees. The one that far away from 90 degrees of the two inclination angles determines the latitude range of the occultation events. 3 LEO－LEO occultation events number reaches a maximum when the heights of TS and RS are the same, and it reaches the maximum when the heights of TS and RS are 600 km . 4 The RAAN of TS and RS has a great influence on the LEO－LEO occultation number, but has little influence on occultation distribution.
结果指出：1对一年掩星事件数量及其纬度分布影响大的轨道参数依次是轨道倾角、轨道高度、升交点赤经和近地点角距；而这些参数对一年掩星事件的经度分布影响都不大；2发射卫星和接收卫星倾角之间的相互关系对掩星事件数量和纬度分布影响最大，两卫星倾角接近互补时掩星事件最多，两颗LEO卫星中与90°相差较大的倾角决定了LEO－LEO掩星事件的纬度分布范围；3发射卫星和接收卫星处于同一轨道高度时，LEO－LEO掩星事件数取得极大值，发射卫星和接收卫星都采用600 km的轨道高度，一年LEO－LEO掩星事件数最多；4 发射卫星和接收卫星升交点赤经的相互关系对LEO－LEO掩星事件数量影响很大，发射卫星和接收卫星升交点赤经之差为120°或240°时掩星事件数量最多，RAAN对掩星事件纬度和经度分布影响不大；5近地点角距对掩星事件数量和分布影响都不大。
- 更多网络解释与轨道倾角相关的网络解释 [注：此内容来源于网络，仅供参考]
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angle of inclination;angle of dip：倾角
"轨道倾斜角","angle of inclination of an orbit" | "倾角","angle of inclination;angle of dip" | "移后角;滞后角","angle of lag"
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angle of inclination of brush：电刷倾角
轨道倾斜角 angle of inclination of an orbit | 电刷倾角 angle of inclination of brush | 入口角 angle of inlet
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orbital inclination：轨道倾角
orbital frequency 轨道频率 | orbital inclination 轨道倾角 | orbit plane 轨道面
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orbital isochronism：等时轨道原理
orbital inclination 轨道倾角 | orbital isochronism 等时轨道原理 | orbital maneuver 轨道操作
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node：交点
轨道的取向表示为轨道平面相对于参考平面[通常为黄道(ecliptic)]的倾角(inclination)以及升交点(node)经度(从春分点到升交点的角距离. 天体在其轨道上的位置则决定于其偏近点角(anomaly),此位置作为时间的函数是从近重心点行程的时间来计算的.
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Persona：角色
这颗名为"角色"(Persona)的军事侦察卫星的地面分辨率最高可达0.25米,工作轨道为210千米×770千米,倾角为98.3. ,周期94分钟,工作寿命超过5年.
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right ascension of satellite ascending node：卫星升交点赤经
02.253 卫星轨道倾角inclination of satellite orbit | 02.254 卫星升交点赤经right ascension of satellite ascending node | 02.255 卫星轨道近地点幅角argument of perigee of satellite orbit
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inclinationofaplanet'sorbit：行星轨道交角
inclinationneedle 倾角指针 | inclinationofaplanet'sorbit 行星轨道交角 | inclinationofbuildingslip 船台坡度