转移轨道

德尔它4系列基于一个公共助推核心有5种构型，能将4233~12757kg规格的中型和重型载荷送入地球同步转移轨道（GTO）。

The delta IV is composed of five configurations based on a common booster core ( CBC ), which is capable of carrying payloads ranging from 4 233 to 12 757 kg into the geosynchronous transfer orbit ( GTO ) .

从空间站起飞直接进入行星际转移轨道的可能性

Possibility of flying directly into interplanetary transfer orbit from space station

使用遗传算法和B平面参数进行月球探测器地月转移轨道设计

Lunar Trajectory Design with GA and B - Plane Parameters

通过建立B平面用迭代方法得到满足要求的月球卫星轨道，并认为定相环形转移轨道的测控优于直接转移轨道。

It shows the phasing loop transfers are better than the direct transfers in the tracking and guidance .

首先就探测器携载GPS接收机用于地月转移轨道近地段定轨的几个问题进行分析；

First the GPS navigation of the lunar probe in the close earth orbit phase is analyzed .

利用简化模型，分析了嫦娥一号飞行器在调相轨道和地月转移轨道的VLBI测角精度。

The precision of CE-1 angle calculation using national VLBI network was analyzed , using a simple Earth rotation model .

通过遗传算法和B平面参数对月球探测器地月转移轨道进行了设计和计算，计算结果表明，结合遗传算法和B平面参数可以很好地解决探月轨道搜索的全局性和快速收敛性问题。

The lunar trajectories are designed and computed by using the method of genetic algorithms and B plane parameters in this paper . The result shows that the iterations of transfer trajectories are wholly and quickly achieved by combining genetic algorithms with B plane parameters .

本研究报告介绍地球同步转移轨道（GTO）被污染情况及其影响，并指出影响GTO上物体轨道寿命几大因素。

This paper describes the GTO pollution and its impact and points out some major perturbative influences on the orbital lifetime of a body in GTO . E.S.

CRTBP模型中的周期轨道在深空探测中有两种可能应用&驻留轨道和转移轨道。

There are two types of possible applications & the target orbits and the transfer trajectories .

现通过对AGA转移轨道的分析，给出了AGA转移轨道设计的拼接条件，此拼接条件是对AGA转移轨道进行设计和分析的重要准则。

In this paper , we analyzed the AGA transfer trajectory and presented the patching conditon for designing the AGA transfer trajectory . This patching condition is the basic principle for designing and analyzing AGA trajectory .

排序算法的探讨击中月球的转移轨道研究

Study of Sorting Algorithm Investigation on Translunar Trajectories for Lunar Impact

日-地系拉格朗日点任务及其转移轨道设计方法

Missions of Sun-Earth Lagrange Points and Design Method of Transfer Trajectory

空间快速响应发射转移轨道设计与制导方法研究

Research on Responsive Space Lift Transfer Orbit Design and Guidance Approach

地月低能转移轨道设计方法研究

Research on Low Energy Transfer Trajectory Design Method Between Earth and Moon

日地平动点卫星两脉冲转移轨道设计

Two impulses transfer trajectory design for Sun-Earth libration point missions

基于平均法的小推力转移轨道优化研究

Optimization of Low-Thrust Transfer Trajectory Based on Averaging Method

多目标进化算法在航天器转移轨道中途修正中的应用

Application of the Multi-objective Evolutionary Algorithm in Midcourse Correction of Spacecraft Transfer Orbit

奔月转移轨道的快速设计方法研究

Study of Rapid Design Method for Cislunar Transfer Trajectory

近地小行星探测转移轨道方案设计与优化

Design and optimize scheme of transfer trajectory for near Earth asteroid exploration mission

基于轨迹成型法星际小推力转移轨道快速设计

A Shape-based Approach to Rapidly Design Interplanetary Low-thrust Trajectories

地球-火星的燃料最省小推力转移轨道的设计与优化

Design and Optimization of Earth-Mars Optimal-Fuel Low-Thrust Trajectory

基于紫外敏感器的地月转移轨道慢旋探测器自主导航算法

Autonomous Navigation Algorithm for Slow-Spin Probe in Earth-Lunar Transfer Orbit Based on Ultraviolet Sensors

航天器进入地球同步转移轨道运行所需速度为10.25公里／秒；

spacecraft Into the geosynchronous transfer orbit speed of 10.25 kilometers requirements / s ;

相位环地月转移轨道研究

Research on Phasing Loops Earth-to-Moon Transfer Orbit

月球探测器转移轨道特性

Some Characteristics of Trans - lunar Trajectory

月球探测器转移轨道的中途修正

Mid-correction of trans-lunar trajectory of lunar explorer

月球探测器地月转移轨道测控技术仿真研究

A Simulation Research on Measurement and Control Technology of Earth-Moon Transfer Orbit of Lunar Probe

首先，基于归一化的改进春分点根数建立了星际小推力转移轨道的优化模型；

First , the optimization model of interplanetary low-thrust trajectory was established using modified equinoctial elements .

考虑月球升交点黄经的地月低能转移轨道

Low Energy Transfer Orbit to the Moon Considering Longitude of the Ascending Node of the Moon

关于地球转移轨道碎片的轨道寿命问题

On Orbit Lifetime of GTO Debris