spacecraft control 中文意思是什麼

spacecraft control 解釋
航天器控制
  • spacecraft : 非載人宇宙飛船
  • control : n 1 支配，管理，管制，統制，控制；監督。2 抑制（力）；壓制，節制，拘束；【農業】防治。3 檢查；核...
  1. Since the technology of intelligent control was first used in the spacecraft in the 60 ' s 20th century by jpl laboratory, the high performance of spacecraft autonomy has been one of the important goals pursued by the spacecraft designing engineer

    從20世紀60年代jpl實驗室將自主智能控制技術應用於航天器以來，盡可能地提高航天器的自主運行水平已是航天器發展的大趨勢。多傳感器信息處理技術是航天器自主運行技術中的重要內容。
  2. Mission control ordered the spacecraft to return to earth

    指揮部命令宇宙飛船返回地球
  3. The spacecraft crew radioed mission control for advice

    太空船機組人員用無線電向任務指揮中心求教。
  4. But if it has power, thorpe said, " the spacecraft is quite capable of autonomous control even if it doesnt hear from earth.

    但如果它的權力，索普說: "飛船尚能自主控制即使不聽到地球
  5. All space craft re - entering the atmosphere get covered in space debris and gases which affect communications between the spacecraft and the ground control center

    所有返航的飛船在進入大氣層時，會被宇宙殘骸和氣體所包圍，從而影響了與地面中心的聯絡。
  6. Study on modeling and simulation of docking control process of some spacecraft

    某型航天器對接控制過程的建模與模擬研究
  7. Europe ' s first spacecraft to the moon ended its three - year mission sunday by crashing into the lunar surface in a volcanic plane called the lake of excellence, to a round of applause in the mission control room in germany

    歐洲第一艘飛月太空船于周日撞擊了月球表面一塊名為「卓越湖」的火山平原，從而結束了其長達三年的探月使命，位於德國的任務監控室里掌聲一片。
  8. Darmstadt, germany ( ap ) - - europe ' s first spacecraft to the moon ended its three - year mission sunday by crashing into the lunar surface in a volcanic plane called the lake of excellence, to a round of applause in the mission control room in germany

    歐洲首架探月飛行器周日撞擊月球表面一片名為"完美之湖"的火山平原，結束了其長達3年的探月任務，德國監控室里掌聲一片
  9. Decoupling sliding mode control in a nonlinear spacecraft system

    非線性空間飛行器系統的解耦滑模控制
  10. Problem formulation, modeling and simulation of the spacecraft attitude and trajectory control. 2

    空間飛行器姿態和軌跡控制問題的數學分析、建模以及模擬。
  11. The applications of real - time system are very popular in modern industrial process, for example, the monitor and management of power system, the flight control of spacecraft, the robot control and the field of force and so on

    在現代工業生產中，實時系統得到廣泛的應用，例如電力監控與管理，航空航天器飛行控制，機器人控制以及軍事領域。
  12. The orbit simulation program mainly concentrates on orbit calculation. this thesis first introduces the fundamental knowledge of orbit dynamics, including orbit perturbation and spacecraft attitude control

    軌道模擬程序核心部分是軌道計算，本文首先介紹了軌道動力學基礎，包括軌道攝動問題，以及飛行器姿態控制等基礎知識。
  13. Abstract : this paper briefly presents th e application of advanced brazing techniques for a larye number of assemblies of space vehicles, such as thrust chamber and turbine rotor of launch rock et engine, titanium tube of satellite, attitude control engine injector and wave guide component of satell ite, reflector, tube and honeycomb panel of manned spacecraft, main engine nozzl e and preburner of space shuttle as well as the pipeline systems of space statio n

    文摘:簡略地介紹了先進釬焊技術在航天器部件，例如運載火箭發動機的推力室和渦輪轉子、人造衛星的鈦導管、姿控發動機噴注器和波導器件、載人飛船的反射器、導管和蜂窩壁板、航天飛機的主發動機噴管和預燃室以及空間站的管路系統等的廣泛應用情況。
  14. This dissertation mainly studies information fusion estimation theory and its application to spacecraft control. the major researching contents of the dissertation are summarized as follows : 1

    本論文就多傳感器系統信息融合估計理論及其在航天器控制中的應用進行了深入研究，所作的主要研究工作有以下六個方面： 1
  15. About the large deformation description, a multi - floating coordinate system is adopted. it can effectively reduce the error of discretization. this paper deals with the design of restrained variable structure control in the way of phase plane analyse, which is concise and avoids complex mathematical descriptions. a new method is promoted for flexible spacecraft control by describing flexible spacecraft dynamics equations as t - s fuzzy model and designing a pdc fuzzy controller

    將撓性航天器姿態動力學方程描述為t - s模糊模型為撓性航天器控制提供了新思路;模擬結果表明，基於t - s模型的pdc模糊控制器能滿足撓性航天器大角度姿態機動的精度要求，並能有效抑制帆板振動，具有一定的智能性。
  16. The current control approaches are based on frequency domain methods such as pid control which assumes linear time invariant system dynamics. the advantages of these approaches are simplicity and ease of stability and robustness analysis. however, the decrease in performanc e and poor efficiency translates to additional payload and cannot meet the demand of current spacecraft control

    當前飛行器主要的控制方法是基於近似時不變線性系統的頻域分析法（如pid控制） ，這種方法的優點是簡單且易於穩定性和魯棒性分析，但它所達到的低性能和低效率卻轉化成了飛行器控制過程的附加載荷，還遠不夠滿足當前飛行器控制的要求。
  17. Controller tuning and testing including stability and robustness analysis. 4. test results to the implementation of mpc for spacecraft control

    對控制器的調試和測試（包括對控制器的穩定性和魯棒性的分析） 。
  18. This thesis studies the spacecraft control using nonlinear model predictive control and computer simulations are applied in it. the main results fall into two main areas. 1

    本文運用非線性模型預測控制理論對空間飛行器位置和姿態的控制進行了系統的分析、研究和計算機模擬，在以下兩個方面取得顯著成效： 1
  19. This dissertation mainly studies information fusion estimation theory and its application to spacecraft control ; automatic diagnosis and system recovery ; strap - down attitude algorithm of fiber optic gyro and its error propagation

    由於慣性系統正由框架式平臺系統逐步向捷聯系統過渡，因此本文還對基於光纖陀螺的捷聯姿態更新演算法進行了研究。
  20. This thesis presents the feasibility of nonlinear model predictive control implemented in spacecraft control and the optimality of increasing the control precision and decreasing the fuels expenditure. and the discussions are then focused on the simulation of spacecraft control using function - space model predictive control algorithm as mentioned below : 1

    本文的主要研究工作是探討非線性模型預測控制（ nmpc ）應用於空間飛行器自適應控制的可行性及對提高控制精度和減少燃料使用方面的優越性，同時利用函數空間模型預測控制演算法（ f - mpc ）對空間飛行器的位置和姿態控制進行模擬，具體內容如下：一
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