orbit control

英 [ˈɔːbɪt kənˈtrəʊl] 美 [ˈɔːrbɪt kənˈtroʊl]

网络  轨道控制; 轨控

计算机



双语例句

  1. Preliminary research on lunar probe orbit control technology based on planar two bodies model and planar polar three bodies model is introduced in this paper.
    进行了基于二体模型和平面三体模型的登月飞行器轨道控制方法的初步研究。
  2. General electric satellite orbit control
    通用电气卫星轨道控制
  3. The orbit control technology of two long-distance satellites with similar semi-major axis, eccentric angle and inclination RAAN was analyzed.
    文章对半长轴、偏心率、倾角、升交点赤经相近的两航天器的远距离轨控接近方案进行了理论分析。
  4. 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.
    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。
  5. Attitude and Orbit Control subsystem which is an important part of a satellite attitude control system is the core components to achieve high-performance attitude and orbit measurement and control.
    姿轨控下位机作为卫星姿轨控分系统的重要组成部分,是卫星实现高性能姿轨测量和控制的核心部件。
  6. For KKV without an orbit control engine along its longitudinal axis, an OGL is developed based on the linear kinematical model of space interception, by adopting a new time to go algorithm.
    针对纵轴方向没有轨控发动机的KKV,建立空间拦截的线性运动学模型,通过采用新的剩余时间计算方法,提出了拦截任意机动目标的最优导引规律。
  7. The simulator has been applied in the simulation and test of small satellite attitude and orbit control system.
    飞轮模拟器已应用于小卫星姿轨控仿真测试系统中。
  8. Research on Modeling and Simulation of Liquid-propellant Rocket Engines with Low Freezing Point Propellant for Attitude and Orbit Control Using Two Mode
    低冰点双模式姿轨控推进系统建模与仿真研究
  9. Simulation platform for the attitude and orbit control system design of small satellites
    小卫星轨道姿态控制系统仿真软件平台
  10. Then, by use of the parameter regulating feedback method, the multi-periodical orbit control of the model and the conversion of the system between the chaos state and orbits of different periods are realized, and the properties of the system can be effectively improved.
    然后运用参数调节反馈控制方法实现了对模型的多周期轨道的控制及系统在混沌态与不同周期轨道间的转换,从而有效地改善了系统的性态。
  11. The rubber materials compatible with propellants were normally used in the dynamic seals of solenoid valves located in thrusters which have beed selected as actuators in spacecraft attitude and orbit control systems at present.
    在航天器中,一般使用推力器作为姿控、轨控执行元件,推力器中的电磁阀动密封常使用和推进剂相容的橡胶材料。
  12. Orbit control is divided into in-plane and out-plane control.
    轨道控制分为平面内轨道控制和平面外轨道控制。
  13. Three Directions in Attitude and Orbit Control Ground Testing System of FY-1C Satellite
    三化在FY-1C卫星姿轨控地面测试系统中的实施
  14. The orbit control and attitude control problems of satellite have been studied in this thesis by use of global differential geometry method.
    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。
  15. The design and realization technology in engineering of the on-board programming for software in satellite attitude and orbit control computer are developed in this paper. The principle of the programming, realization, reliability design, resource distribution, joint requirement and operation process are presented.
    对卫星姿轨控计算机软件在轨编程功能的设计和工程实现技术进行了研究,给出了在轨编程的原理、实现方法、可靠性设计、资源分配、接口要求和在轨编程的操作步骤。
  16. To meet the need of on-board computer-in-the-loop simulation, real-time simulation system for attitude and orbit control of a flexible satellite is designed based on dSPACE multiprocessor system.
    为满足某在研大型挠性卫星计算机在回路中的仿真需要,利用dSPACE多处理器系统设计了卫星姿态和轨道控制实时仿真系统。
  17. With advantages of simple and reliable in structure, high Isp and easy control over a wide range of thrust, Pulsed Plasma Thruster ( PPT) is very suitable for micro-satellite's orbit control and high precision attitude control.
    脉冲等离子体推力器(PPT)具有结构简单可靠,比冲高,推力在较大范围可控的特点,适合用于微、小卫星轨道控制和小卫星高精度姿态控制,其研究和应用得到了重视。
  18. Constellations and Their Orbit Control Techniques
    星座与星座轨道控制技术
  19. 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.
    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。
  20. When the mass of the spacecraft becomes very small, its propulsion system should be light in weight and precise in thrust for high precision attitude maneuver and orbit control.
    当航天器的质量非常小的时候,其推进系统必须具有质量轻,精度高的特点,以适应精确的轨道控制和姿态调整;
  21. 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.
    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。
  22. With the continuous development of the satellite technology and increase of the system complication, the design of software architecture for the Attitude and Orbit Control System of satellite has become an important problem.
    随着卫星技术的不断发展和系统复杂性的不断提高,姿轨控系统软件体系结构的设计成为卫星姿轨控系统一个重要的研究课题。
  23. On Orbit Control of Spacecraft around Collinear Libration Points
    关于探测器定点在共线平动点附近的控制问题
  24. The rendezvous and docking ( RVD) between two spacecrafts in space involves both orbit control and attitude control with up to12 degrees of freedom.
    空间交会对接涉及到两个航天器同时要进行多达12个自由度的轨道和姿态控制问题。
  25. Given orbit control and attitude control engine thrust model.
    接着给出了轨道控制小推力火箭发动机的推力模型,并讨论了弹体上发动机的分布布局。
  26. The project shows good autonomous and robust performances from the simulation results. Third, the relative orbit control, attitude control and the rendezvous safety questions of near-distance rendezvous are studied.
    再次,研究了近程交会相对轨道控制、姿态控制及交会安全问题。
  27. The proposed optimal rendezvous strategies both for long-distance elliptical rendezvous trajectory and near-distance elliptical rendezvous trajectory and terminal guidance laws will provide technique support for the space rendezvous scheme design and orbit control of OMV.
    论文提出的椭圆远程、近程最优交会策略和末制导导引律可为轨道机动飞行器空间交会方案设计与轨道控制提供技术支撑。
  28. Taking into account the Coupled attitude and orbit control of the Kinetic energy interceptor, this article carries out the simulated shooting test of the target under different Mobile forms and analyzes the impact of different forms of mobility to the miss distance.
    在考虑动能拦截器姿轨控耦合的情况下,对不同机动形式的目标进行了模拟打靶试验,并分析了不同机动形式对脱靶量造成的影响。
  29. The control of Lorenz-Haken laser chaos is realized by using the shooting method, including the periodic orbit control and stability control.
    通过用打靶法对Lorenz-Haken激光混沌模型进行控制,包括周期轨道控制和稳定轨道控制。