深空探测器的英文

• deep space probe

• "深"英文翻译    deep
• "空"英文翻译    leave empty or blank; empty; ...
• "探测器"英文翻译    finder; detector; seeker; so ...
• "深空探测设备" 英文翻译 :    deespace instrumentation facility (dsif)
• "深空探测系统" 英文翻译 :    deep space instrumentation system
• "陆空探测器" 英文翻译 :    air-ground detection
• "太空探测器" 英文翻译 :    deep-space probe; probe; space; surveyor
• "空对空探测器" 英文翻译 :    air-to-air detector
• "深空间探测器跟踪" 英文翻译 :    deep space probe tracking
• "无线电高空探测器" 英文翻译 :    radiosonde
• "低空探测" 英文翻译 :    low-altitude detection
• "对空探测" 英文翻译 :    air detection
• "高空探测" 英文翻译 :    aerologic sounding; aerological ascent; aerological obserbatory; aerological sounding; sound ranging; u er air soundings; upper air soundings; upper-air sounding
• "高空探测站" 英文翻译 :    u er-air （sounding） station; u er-air（sounding）station; upper-air station
• "太空探测" 英文翻译 :    space exploration
• "越空探测" 英文翻译 :    transosonde
• "低空探测雷达" 英文翻译 :    lacr low altitude coverage radar
• "对空探测能力" 英文翻译 :    air detection capability
• "防空探测雷达" 英文翻译 :    defense acquisition radar
• "飞机高空探测" 英文翻译 :    airplane sounding
• "高空探测火箭" 英文翻译 :    high-altitude rocket; rockair; rockoon; sky rocket; skyrocket; sounding vehicle
• "高空探测技术" 英文翻译 :    altitude acquisition technique
• "高空探测装置" 英文翻译 :    sonde
• "探测器" 英文翻译 :    finder; detector; seeker; sounder; probe
• "检测器，探测器" 英文翻译 :    detector

• Application of universal variables to designing deep - space probe orbit
  普适变量法在深空探测器轨道设计中的应用
• This thesis deeply researches the virtual reality techniques used in the spacecraft ’ s soft landing process on asteroids
  本文对深空探测器在小行星表面软着陆过程中一些虚拟现实技术进行较为深入的研究。
• Based on the scheme of exploration ivar asteroid , this dissertation studied the mission planning technology and system design
  本文基于探测ivar小行星的设计方案,对深空探测器自主任务规划方法和系统设计进行了研究。
• In recent ten years , countries all over the world have launched numbers of deep space probes to explore various kinds of valuable celestial bodies in the solar system
  最近的数十年中,世界各国发射了许多深空探测器,用以探测太阳系内有科学价值的各类大小天体。
• As the modern small satellite technique developing quickly , the multifunctional structure ( mfs ) technique is come out . the mfs technique is a new designed method of deep space detector
  多功能结构技术是在现代小卫星技术飞速发展的情况下,而兴起的一种新的深空探测器设计方法。
• With the development of our spaceflight and progress of deep space exploring , the conflict in the deep space detector between large numbers of data to be transmit and limited channel capability is more and more serious
  随着我国航天事业的进步和深空探测活动的开展,深空探测器中大量的数据传输需求与有限的信道容量之间的冲突亟待解决。
• For deep space explorer , the attitude control system design methods were studied in this dissertation , which is funded by the national 863 plan ( 2004aa735080 ) , “ autonomy technology and simulation demonstration system for deep exploration ”
  本文结合国家863科研计划项目“深空探测自主技术与仿真演示系统” ( 2004aa735080 ) ,对深空探测器姿态控制系统设计方法进行了研究。
• The main contents of this dissertation consisted of the following parts : the dynamics mathematic model for the deep space explorer is building up . the compositions and features of environmental torques were analyzed during interplanetary cruise period
  主要工作包括:建立了深空探测器的动力学模型,针对其星际巡航段分析了其环境干扰力矩的组成和特性,得出太阳光压力矩是其主要干扰力矩的结论。
• To verify the validation of modeling design , the paper modeled a deep space explorer with a deep space mission . analyzing and validating the planning model . in order to realize fleetly modeling and modeling with intelligent , this paper proposed “ stencil - plate ” mode of modeling
  为了进一步验证本文建模设计的有效性,文中以深空探测器某一任务段为应用实例,建立探测器自主规划模型,并对所建立的模型做了规划验证。
• The result shows that the solar radiation pressure moments play a mainly part . based on kalman filtering , three kinds of attitude determination algorithms were studied using the attitude sensor now available on the explorer : the first based on digital solar sensor ( dss ) and gyroscope when the star sensor is not available ; another based on dss , high - gain antenna ( hga ) and gyroscope when the explorer is in the earth - safe mode ; the third based on star sensor combined with gyroscope when the explorer is in the normal mode
  针对配置了典型测量敏感器的深空探测器,基于扩展kalman滤波给出了其姿态确定的方法:针对星敏感器不可用情形,给出了使用太阳敏感器和速率陀螺定姿的滤波器算法;针对安全模式下的对地稳定定向情形,给出了太阳敏感器和高增益天线融合速率陀螺信息的定姿算法;针对正常巡航模式给出星敏感器和速率陀螺联合定姿算法。