深空探測器 的英文怎麼說

中文拼音 [shēnkōngtàncèqì]
深空探測器 英文
deep space probe
  • 深 : Ⅰ形容詞1 （從上到下或從外到里的距離大） deep 2 （深奧） difficult; profound 3 （深刻; 深入） thor...
  • 空 : 空Ⅰ形容詞（不包含什麼; 裏面沒有東西或沒有內容; 不切實際的） empty; hollow; void Ⅱ名詞1 （天空） s...
  • 探 : Ⅰ動詞1 （試圖發現） try to find out; explore; sound 2 （看望） call on; visit; see 3 （向前伸出）...
  • 測 : 動詞1. （測量） survey; fathom; measure 2. （測度; 推測） conjecture; infer
  • 器 : 名詞1. （器具） implement; utensil; ware 2. （器官） organ 3. （度量; 才能） capacity; talent 4. （姓氏） a surname
  • 探測器 : finder; detector; seeker; sounder; probe
  • 探測 : survey; search; sound; probe; sounding; detection; acquisition; reconnaissance; localization; fin...
  1. In perhaps the most unusual proposal of all, scientists from nasa ' s jet propulsion laboratory ( jpl ) in california are proposing to build a probe that uses heated water jets to descend to depths of up to a hundred meters through the frozen ice caps at the martian poles inn search of organic matter

    在或許是最不一般的建議的倡導下，加利福尼亞州航空航天局噴氣推進實驗室（ jpl ）的科學家們正在計劃建造一臺探測器，使用熱水射流穿透火星極地的冰帽，深入到100米以下，搜尋有機物質。
  2. Application of universal variables to designing deep - space probe orbit

    普適變量法在深空探測器軌道設計中的應用
  3. Because of the long distance of exploration targets and the non - determinacy of flight environment in deep space exploration, a key problem proposed is how to control and operate the deep space explorer reliably and in real time

    深空探測由於探測目標距離遠，飛行環境不確定等因素，給探測器的控制和操作帶來了實時性和可靠性的問題。
  4. 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

    針對配置了典型測量敏感器的深空探測器，基於擴展kalman濾波給出了其姿態確定的方法:針對星敏感器不可用情形，給出了使用太陽敏感器和速率陀螺定姿的濾波器演算法;針對安全模式下的對地穩定定向情形，給出了太陽敏感器和高增益天線融合速率陀螺信息的定姿演算法;針對正常巡航模式給出星敏感器和速率陀螺聯合定姿演算法。
  5. For the autonomous spacecraft is very complicated, carrying overall mathematical simulation to such a system is very difficult to realize by one computer only. according to the system ' s own characteristics, we can adopt hla ( high level architecture ) structure, distributing the simulation task to the nodal computer of each network

    根據探測器自主系統特點，本文將高層體系結構（ hla ， highleverarchitecture ）應用於深空探測自主技術模擬中，將模擬任務分佈到各個網路節點計算機上，實現了分散式的深空探測自主技術的模擬系統。
  6. 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 ”

    本文結合國家863科研計劃項目「深空探測自主技術與模擬演示系統」 （ 2004aa735080 ） ，對深空探測器姿態控制系統設計方法進行了研究。
  7. This thesis deeply researches the virtual reality techniques used in the spacecraft ’ s soft landing process on asteroids

    本文對深空探測器在小行星表面軟著陸過程中一些虛擬現實技術進行較為深入的研究。
  8. Based on the scheme of exploration ivar asteroid, this dissertation studied the mission planning technology and system design

    本文基於探測ivar小行星的設計方案，對深空探測器自主任務規劃方法和系統設計進行了研究。
  9. 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

    最近的數十年中，世界各國發射了許多深空探測器，用以探測太陽系內有科學價值的各類大小天體。
  10. 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

    多功能結構技術是在現代小衛星技術飛速發展的情況下，而興起的一種新的深空探測器設計方法。
  11. 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

    隨著我國航天事業的進步和深空探測活動的開展，深空探測器中大量的數據傳輸需求與有限的通道容量之間的沖突亟待解決。
  12. 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:建立了深空探測器的動力學模型，針對其星際巡航段分析了其環境干擾力矩的組成和特性，得出太陽光壓力矩是其主要干擾力矩的結論。
  13. 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

    為了進一步驗證本文建模設計的有效性，文中以深空探測器某一任務段為應用實例，建立探測器自主規劃模型，並對所建立的模型做了規劃驗證。
  14. In deep space exploration missions, autonomous navigation technology is very important, and in this paper, we do some research into the autonomous navigation schemes of encountering small celestial bodies. it is mainly described as the follows : firstly, by analyzing the orbit characteristics and task requirements in encounter, the simplified orbit dynamic model for the deep space probe is built up, and whether the corresponding model error that meets the demanding of autonomous navigation task is validated

    在深空探測任務中，自主導航技術是十分重要的，本文對交會小行星的自主導航方法進行研究，主要內容包括:首先，分析交會小行星的軌道特性及任務需求，建立簡化的深空探測器軌道動力學模型，並驗證了簡化模型的誤差能否滿足自主導航任務的需求。
  15. In the 21st century, aerospace countries will focus all their attention on deep space exploration. real - time control and operation of the spacecraft becomes a difficult problem because of the factors, including long distance away exploration targets and uncertain flight environment

    深空探測是21世紀世界宇航大國關注的焦點，由於深空探測的目標遠、飛行環境不確定等因素，使探測器的實時控制和操作成為難題。
  16. Observers that are used for deep - space exploration are often deployed without any defensive systems

    用於深空探測的觀察器常常沒有任何防禦系統。
  17. This paper presents and probes into several filtering schemes for the deep space explores attitude measurement system composed of star sensors and gyros. under the stellar - inertial modes, two attitude determination algorithms are designed which use the extended kalman filter. one of the algorithms is to linearized the state equation based on the optimal estimation

    本文中以星敏感器和光纖陀螺為基本配置組成的深空探測器姿態測量系統為對象，針對星敏感器與光纖陀螺聯合定姿模式和基於星敏感器的定姿模式，對深空探測器的三軸姿態濾波技術方案進行了設計與研究。
  18. Defining the states and resources and activities of the system by template. the planning experience is carried out on this software platform by taking example for a section of flight mission target of the deep space exploration

    該平臺實現了以模板化的建模方式對探測器的資源、狀態變量、任務活動進行定義，在此平臺基礎上，以深空探測飛行過程中的某一任務目標為例，進行了應用。
  19. In the end, to realize modeling using the template in this paper, simulation system of modeling and mission planning for deep space explorer is designed and realized with java language

    為實現探測器自主規劃系統建模的快捷化和智能化，本文提出了模板化的黑箱建模方式。最後，採用java語言，設計並實現了深空探測任務建模/規劃系統平臺。
  20. Firstly, this dissertation studies three key problems in autonomous mission planning of the deep space explorer, including task serial planning, asteroids selection and planning for autonomous optical navigation and large angle slew planning of the explorer. based on the solution of these problems, autonomous mission planning system of the deep space explorer is preceded

    本文先對深空探測器自主任務規劃中的三個關鍵問題? ?任務序列的規劃、導航小行星的篩選與規劃、探測器大角度機動規劃進行了深入的研究，在解決這三個問題的基礎上，進行了深空探測器自主任務規劃系統的設計。
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