各地的您选择的驱动当然，你看比赛采取的轨道控制…
Race around the course with your choice of driver as you look to take control of the track…
本文介绍了将智能控制方法用于航天器交会对接段的轨道控制。
The method of intelligent control applied to the orbital control of rendezvous and docking phase of spacecraft is presented in this paper.
因此，必须建立一套良好的测量体系以及精确的无砟轨道控制网。
So, we should found a suit of favorable survey system and the precise control networks.
描述许多轨道控制问题的方程通常构成非线性半显式的微分代数系统。
The equations which describe many trajectory control problems naturally form nonlinear semiexplicit differential algebraic systems.
本文利用整体微分几何的方法研究了人造卫星的轨道控制和姿态控制问题。
The orbit control and attitude control problems of satellite have been studied in this thesis by use of global differential geometry method.
根据姿态控制推力器的输出特性，设计了轨道控制期间卫星姿态控制方案。
The attitude control law is designed for the orbital maneuver with considering the output character of the attitude control thrusters.
针对近距离相对运动的轨道控制问题，提出用常值小推力完成最优转移的方法。
An optimal orbit maneuver method based on continuous low thrust was presented to solve relative motion control.
卫星轨道控制期间，轨道控制推力会激振挠性太阳帆板，从而也影响卫星的姿态。
When the satellite takes orbital maneuver, the control force may stimulate the vibration of the flexible appendages and, therefore, affects the attitude of the satellite.
应用卫星绝大部分都是近圆轨道的卫星 ，其中又有很多是需要进行轨道控制的。
Most of application satellites are running in near circular orbits, and many of them need to be controlled.
提出了一种通过控制平均轨道控制目标对应的瞬时轨道偏差量进行轨道修正的方法。
An orbital modulation method by controlling the corresponding transient orbit errors of mean orbit control targets was proposed.
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。
The result of quantitative analysis shows that the method is feasible, and be helpful for the research of orbit design and control.
为了保证冻结轨道的冻结特性，平面内轨道控制需要对半长轴、偏心率和近地点幅角都控制。
In order to guarantee the characteristics of frozen orbit, in-plane orbit control needs to adjust the semi-major axis, eccentricity, argument of perigee simultaneously.
序列编辑器允许你排队模式，发挥每个轨道控制的任何安排，使图案，并迅速混音工程的重用。
The sequence editor allows you to queue patterns to play for each control track in any arrangement, enabling reuse of patterns and quickly remixing projects.
基于定轨误差、轨道控制误差和轨道预报误差的调相时间分析，制定了目标飞行器调相控制策略。
Based on the target's phasing time analysis of orbit determination error, orbit control error and orbit prediction error, the strategy of the target's phasing orbit maneuver was developed.
随着小卫星应用领域的日益广阔和小卫星数量的不断增长，对小卫星轨道控制技术的要求也越来越高。
With the wide application of small satellite and its increasing quantity, the requirements for orbit control technology of the small satellite is becoming more strict.
井眼轨迹控制是侧钻水平井技术的核心，而轨道设计与优化设计又是轨道控制技术的两大关键技术之一。
The control of the trajectory is the core technique in horizontal well technique, while trajectory design and optimal design are the two key techniques.
进行了基于平面三体模型的登月飞行器轨道控制方法的研究；研究了从近地低轨道到近月低轨道的飞行轨道；
The flight trajectories from low earth parking orbit (LEO) to low lunar parking orbit (LLO) based on a planar three-body model are studied.
进而导出了带有J2项摄动的环绕星相对运动方程，并给出了基于惯性笛卡尔坐标系运动学变量的相对轨道控制方法。
Then a control method considering the J2 perturbation based on Encke's linearization equation is proposed to maintain the relative motion of the constellation.
本文导出了基于对象CARMA模型的多变量广义预测自适应控制器，并将这种新的控制方法应用于航天器轨道控制中。
It is presented in this paper a multivariable generalized predictive adaptive controller based on CARMA model and its application in the orbit control of spacecraft.
由于采用了一种新的剩余时间算法，在空间拦截弹的弹体纵轴方向无轨道控制发动机的情况下，也可以实现这种最优导引规律。
For a new time-to-go algorithm, the optimal guidance law can be realized without a trajectory control engine along the lengthwise axis of the missile.
根据卫星在轨运行数据，给出了卫星在轨运行的部分曲线和姿态控制、轨道控制的指标实现情况，对姿态控制分系统方案进行了在轨验证。
According to operation data of the satellite on orbit, some operation results and the specification conformity are presented. Furthermore, the control system scheme is demonstrated on orbit.
届时地面控制人员将点燃助推器，把卫星送入预定轨道。
Ground controllers will then fire the booster, sending the satellite into its proper orbit.
一旦连接到轨道上，汽车将由系统提供电力，由中央计算机控制。
Once attached to the rail, the car will become electrically powered from the system, and control of the vehicle will pass to a central computer.
在太阳引力的控制下，每个行星都维持在一条椭圆形的轨道上，并按照相同的方向移动。
Under the control of the Sun's gravitational force, each planet maintains an elliptical orbit and all of them travel in the same direction.
印度在2008年将一颗卫星发射至月球轨道，不过在一年后，由于卫星通讯突然中断，科学家失去了对其控制而不得不将之抛弃。
India launched a satellite into moon orbit in 2008, but had to abandon it nearly a year later after communication links snapped and scientists lost control of it.
宇航员返回地球之后，BX - 1实施了主动控制，并通过命令向留在轨道上的轨道舱返回。
After the taikonauts had returned to Earth, the BX-1 was placed under active control and commanded to maneuver back towards the orbital module, which had been left in orbit.
理论技术包括播撒雨种降雨、利用生物可降解浮油控制水汽蒸发和轨道加热。
Theoretical techniques include seeding to cause rain, controlling evaporation with a biodegradeable oil slick and heating from orbit. Credit: David Fierstein
日本宇宙开发机构的津田雄一说：“借助智能玻璃，我们只要利用太阳光就可既控制飞行轨道又控制飞行姿态。”
"With this we can control both the orbit and the attitude using only sunlight," says Yuichi Tsuda of the Japan Aerospace Exploration Agency.
你们如何控制空间站在自己的轨道上运行？
你们如何控制空间站在自己的轨道上运行？
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