目标飞行器

  • 网络target spacecraft
目标飞行器目标飞行器
  1. 某目标飞行器真空热试验操作平台设计

    Platform design for vacuum thermal test of the a target spacecraft

  2. 目标飞行器位置姿态的光学测量

    Optical measurement of position and attitude for target spacecraft

  3. 9月29日,中国在酒泉卫星发射中心用长征二号F运载火箭将天宫一号目标飞行器发射升空。

    A screen shows the blast-off of the Long March-2FT1 carrier rocket loaded with Tiangong-1 unmanned space lab module at Beijing Aerospace Control Center , Sept.29,2011 .

  4. 通过对安装在目标飞行器上的四个共面编码标志的测量,来实时计算追踪飞行器上CCD相机的外参数。

    The exterior parameters of the CCD on the chase aircraft can be calculated in-phase by measuring four targets in a place on the target aircraft .

  5. 在航天器姿态动力学与控制仿真框架基础上研制了RVD目标飞行器仿真的原型系统。

    The prototype of RVD target-spacecraft simulation system is built up as ai application example of the object-oriented spacecraft attitude simulation framework .

  6. 交会对接目标飞行器姿态动力学与控制仿真研究

    Attitude Dynamics and Control Simulation for RVD Target-Spacecraft

  7. 分析相机与目标飞行器之间的相对运动造成的像移误差对于测量的影响。

    Impact of error leaded by image motion caused by relative movement between camera and target aircraft is considered .

  8. 项目发言人称,“天宫一号”将作为空间交会对接的目标飞行器,完成交会对接试验。

    The program spokesman said that Tiangong-1 will serve as " a target spacecraft " for rendezvous and docking experiments .

  9. 我国载人航天二期工程研制的交会对接目标飞行器由实验舱和资源舱组成。

    Target spacecraft in the second phase of national manned astronautical engineering , consists of resource cabin and experimental cabin .

  10. 中国计划在2011年下半年发射无人目标飞行器“天宫一号”,并完成中国首次空间交会对接任务。

    China plans to launch an unmanned space module , Tiangong-1 , in the second half of2011 for the nation 's first space docking .

  11. 在本文中以微分对策为基础,研究了导弹-目标飞行器在碰撞轨线附近的三维空间拦截问题。

    In this paper , the problem of interception of missile-traget aircraft has been studied in three dimensional nearby collision-course based on differential game theory .

  12. 接下来几天,“天宫一号”目标飞行器的各个系统将接受综合的质量检查,并完成燃料的加注工作。

    The " Tiangong-1 " target spacecraft will receive comprehensive quality review on all of its systems and complete fuel filling in the next few days .

  13. 天宫一号目标飞行器与神舟八号飞船先后成功发射并顺利交会对接,成为我国载人航天发展史上新的里程碑。

    The Tiangong-1 space module and the Shenzhou-8 spacecraft were launched , and Shenzhou-8 successfully docked with Tiangong-1 , marking a new milestone in China 's development of manned spaceflights .

  14. 本文工作有助于加快交会对接目标飞行器的研制进度,并为其它航天器的结构设计提供了有益参考。

    The work in this thesis can speed up the development schedule of the rendezvous and docking target spacecraft . The method and conclusions would be available for the design of other spacecraft .

  15. 中国正在为将首名女航天员送入太空做准备,这次飞行也是中国的宇宙飞船与天宫一号目标飞行器进行的首次载人交会对接任务。

    China is getting ready to send a woman into space for the first time in a mission that will also represent the country 's first manned docking mission with its Tiangong-1 space station .

  16. 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 .

  17. 根据目标飞行器轨道高度和追踪飞行器入轨轨道高度,给出了目标飞行器交会对接轨道初始相位的设计方法。

    According to the target spacecraft ′ s orbit height and the chaser spacecraft ′ s orbit height , the design method of the target ′ s initial phase for the rendezvous orbit was presented .

  18. 首先根据严格的中心投影共线条件方程,推导出目标飞行器光学特征点坐标和对应的像点坐标与内参数及相对位置和姿态的严格解析关系;

    At first , in the paper the rigorous analytical relations among the feature point coordinates of the target spacecraft , the corresponding image point coordinate , interior parameters , relative position and pose are induced according to rigorous collinear equation of the central projection .

  19. 本文针对跟踪慢速活动目标飞行器两类测量数据的特点,分别采用不同的滤波估值方法,能较精确地确定目标的位置和导引攻角的传递系数。

    According to two kingds of measuring data distinguishing features of vehicle two different filtering and estimation methods for tracking low speed target are provided in this paper , with them the location of target and the transfer coefficient of steering attack angle are confirmed accurately .

  20. 一种针对运动目标的飞行器航迹搜索算法

    A route planning algorithm for unmanned air vehicle towards moving target

  21. 攻击固定目标的飞行器制导控制一体化设计

    An Integrated Approach to Guidance and Control for Aircraft Applying to Attack the Ground Fixed Targets

  22. 对于攻击地面固定目标的飞行器,提出一种非线性制导律和控制方法。

    A nonlinear guidance law and control strategy is proposed for aircraft applying to attack the ground fixed targets .

  23. 本文运用飞行力学原理和现代控制理论,对攻击地面固定目标的飞行器的再入机动制导方法进行了研究。

    In this paper , the method of reentry maneuver guidance applying to attack the ground fixed target is described by using flight dynamics principle and modern control theory .

  24. 研究目标与试验飞行器

    Research target and test vehicle

  25. 分析对比了空间目标与可控飞行器轨道确定的不同,论述了太阳翼定向模式的不同对轨道运动特性的影响。

    The orbit determination difference between space target and controllable vehicle are compared and analyzed , the solar wing orientation mode and it ′ s influence to orbit is discussed .

  26. 针对空间飞行器自主交会对接的要求,研究了利用卡尔曼滤波估计非合作目标交会的飞行器运动状态的方法;

    Considering the request of spacecraft 's automatic rendezvous and docking with a non-cooperative target , a method of estimating the motional state with the incomplete observing information based on Kalman filter is investigated .

  27. 亚马逊在美国和英国都有无人机测试中心。去年该公司表示,正在创建AmazonPrimeAir服务,其目标是利用无人飞行器将包裹送到数百万顾客手中,顾客下单后最多等半小时包裹即可送到。

    The company , which has drone R & D testing centres in both the US and the UK , said last year that it was creating Amazon Prime Air , which aims to use pilotless flying vehicles to deliver packages to millions of customers within half an hour of orders being placed .

  28. 应用多目标决策理论为飞行器总体方案的确定提供了一个决策方法。

    This paper presents a method for defining general scheme of microlight aircraft using multiobjective decision making .

  29. 本文在建立空间飞行器模拟件参数优化的数学模型的基础上,将模糊多目标决策理论用于飞行器模拟件的结构参数优化,提出了一种新的模糊评价指数。

    On the basis of establishing a mathematic model for the parameter optimization of the aircraft simulator , a fuzzy multi-objective decision-making theory is applied to optimizing its structural parameters , and new fuzzy evaluation indices are proposed .