Micro satellite is under the influence of perturbative forces which would affect its orbit, so it is important to consider these perturbations in micro satellite orbit design and control.
小卫星在实际运行中受到多种摄动力的作用，这会对其轨道造成不同程度的影响，因此在小卫星的轨道设计与控制中，摄动是必须考虑的重要因素。
This study is of high value for orbit design for lunar exploration.
研究结果对探月轨道设计有一定的参考价值。
Have some research on the orbit design of the Distributed Spaceborne SAR System.
对分布式星载干涉SAR的轨道设计进行了研究。
Near-field autonomous rendezvous orbit design problem is discussed by adopting CW equation in the paper.
采用线性化CW方程研究了空间飞行器近程自主交会轨道设计问题。
Some basic principles for orbit design of lunar probes are discussed while compared to launching the satellite around the earth.
分析了月球探测轨道设计与地球卫星的区别，给出了一些最基本的设计原则。
Based on the summarization of the orbit design methods, a wizard designer making use of module method was designed in this paper.
文中在对航天器轨道设计方法归纳总结的基础上，采用组件方式设计了向导式轨道设计器。
The result of quantitative analysis shows that the method is feasible, and be helpful for the research of orbit design and control.
定量分析结果表明，该方法切实可行，可以为轨道设计和轨道控制研究工作提供参考。
So both methods of orbit design are suitable for designing orbit of concomitant satellite formation flying around the space station.
用动力学和运动学两种方法研究空间站伴随卫星编队飞行的轨道设计。
Particularly, the method of coverage orbit design is given in view of the orbital period deviation, which is based on recursive orbit.
特别是，以循环轨道为基础，考虑轨道周期的误差，给出覆盖轨道的设计方法。
The proposed model, control strategy and analysis methods are applicable to the target′s rendezvous orbit design and control implementation.
所提出的计算模型、控制策略和分析方法适用于目标飞行器交会对接轨道设计和控制实施。
Introduce the reference frame and time system used in orbit design particularly. Analyzed the orbit characteristic of two-body problem and launch window.
详细介绍了用于轨道设计的坐标系统和时间系统，分析了二体轨道特性和发射窗口的基本特性。
In this paper, a series of characters for recursive orbit and coverage orbit of satellites are discussed, and the method of recursive orbit design is given.
本文阐述人造卫星循环轨道与覆盖轨道的一系列性质，给出确定循环轨道的方法。
Circular arc well section parameter calculation is the most primary question among a series of questions of directional orbit design and actual surveyed trajectory.
在定向井轨道设计、实钻轨迹监控等一系列问题中，圆弧井段参数计算是一个最基础的问题。
With the difficulty of measuring relative velocity considered, a relative orbit design method is proposed to obtain diverse relative orbits with only position feedback.
为了得到更丰富的相对轨道，同时考虑到相对速度测量困难，研究了仅利用位置反馈进行相对轨道设计的方法。
According to characteristic of regional exploring satellite system, an intermittent regional covering orbit design scheme is proposed using circular sun synchronization orbit.
根据区域性探测卫星系统的特点，提出了利用太阳同步轨道间歇性区域性覆盖特定区域的轨道设计方案。
Considering constraints of energy, time and line-of-sight angle, a near-range autonomous rendezvous glidescope orbit design method is studied based on the differential equation method.
考虑能量、时间、视线等约束条件，基于微分方程法研究了近程自主交会滑移轨道设计方法。
This paper has discussed "a small assistant" 's design method and skill in multimedia software from three respects such as element design, dynamic result design and sport orbit design, etc.
本文从图像元素设计、动态效果设计、运动轨迹设计三个方面，讨论了多媒体软件中“小助手”的设计方法和技巧。
Combining the imaging principle of Spaceborne SAR, this paper deduce some conclusions about the orbit design of the Distributed Spaceborne SAR, and in conclusion gives the design way of it.
结合星载干涉SAR成像机理，推导出分布式星载干涉SAR轨道设计中，轨道参数应该满足的基本约束条件，并以此为基础给出了分布式星载干涉SAR轨道设计的一般方法。
The coupling relationship and associated effect among orbit design, satellite design and launch determination in the satellite system design were analyzed, and the simplified MDO module was founded.
分析了卫星总体设计中轨道设计、卫星设计和发射选择间的耦合关系与协同效应，建立了MDO的简化模型。
The coupling relationship and associated effect among orbit design, satellite design and launch determination in the satellite system design were analyzed, and the simplified MDO module was founded.
分析了卫星总体设计中轨道设计、卫星设计和发射选择间的耦合关系与协同效应，建立了MDO的简化模型。
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