launch vehicle system 中文意思是什麼

launch vehicle system 解釋
運載火箭上的系統
  • launch : vt 1 使（船）下水。 launch a ship from a shipyard 使船從船塢下水。2 發射；投出；提出，發出。3 （...
  • vehicle : n. 1. 車輛；載運工具；飛行器；運行工具。2. 媒介物，媒質。3. 【藥學】賦形劑。4. 【繪畫、化】展色料，載色劑。
  • system : n 1 體系，系統；分類法；組織；設備，裝置。2 方式；方法；作業方法。3 制度；主義。4 次序，規律。5 ...
  1. Ground test equipment training simulation system based on off - ballistic trajectory measure and wireless security system of launch vehicle

    運載火箭外測安全系統地面測試設備模擬訓練系統
  2. This section essence shrinks the proportion is 1 : 43 simulation model vehicle the east wind - 11 short distance trajectory guided missile truck which develops voluntarily by our country, may mobile launch carries the system is a prototype, the chassis and the missile are the alloy manufacture, the missile may take out from the discharger or revolves along with the discharger to each angle, all vehicle doors may open, the rubber tire may rotate, the zero number of articles approaches 200

    此款精縮比例為1 : 43的模擬模型車以我國自行發展、可機動發射的東風- 11短程彈道導彈車載系統為原型，車體及導彈為合金製造，導彈可以從發射架上取出或隨發射架旋轉至各個角度，所有車門均可打開，橡膠輪胎可以轉動，零件數接近200個。
  3. Fifth, vpm is real - time digital simulation system software of launch vehicle and missile

    5 、 vpm是運載火箭和導彈的實時數字模擬軟體系統。
  4. The paper has founded the model of laser transmission in launch process and the movement model of laser - powered vehicle, and has analyzed the influence on performance of launch system, which was raised by some factors, for instance, the performance of thruster, the attenuation in transmission, the height of mode - transform, the laser power, the air drag force, the launch height, and so on

    本文研究了激光推進微小衛星發射系統的概念和性能。建立了發射過程激光傳輸和激光推進運載器運動模型，分析了推進系統性能、大氣傳輸衰減、模式轉換高度、激光器功率、大氣飛行阻力、發射點高度等因素對發射系統性能的影響。
  5. This paper relies on country 863 project " taking off levelly, two stage to orbit and transatmosphere flight vehicle system design ", research towed flight dynamics primarily, development for our country air launch technology of carrier rocket, offering the essential technological reserve

    本論文以國家863項目「水平起飛兩級入軌跨大氣層飛行器總體設計」為依託，對牽引飛行動力學進行初步研究，為我國研究運載火箭空中發射技術提供必要的技術儲備。
  6. Use energy - based control method to achieve the entry flight control of reusable launch vehicle. the basic concept is to take the energy as primary control variables, reduce the order of the system and design a tracking law to follow a three - dimensional entry trajectory

    本文採用基於能量的控制方法實現對航天器再入軌跡的控制，將能量作為獨立參量，從而降低系統的階數，利用線性反饋的方法設計一個跟蹤三維再入軌跡的控制律。
  7. The study of launch vehicle platform align emulation system

    運載火箭初始對準模擬系統的研究
  8. Some technique issues concerned to the scene simulation system of the launch vehicle was discussed and developed in this thesis. in this scene simulation system, the established 3 - dimension ( 3d ) model of the objects are imported to scene simulation environment by programming to create a vivid virtual scene. scene simulation technique can objectively describe the simulation process, realize the flight simulation as well as real time roam of launch vehicle, etc.

    其中，視景模擬系統是整個系統最有顯示度的部分，它採用視景模擬技術，根據模擬的目的，構造模擬對象的三維模型和場景驅動，達到客觀、實時的再現模擬過程，實現火箭飛行狀態的可視化模擬和火箭測試狀態的實時漫遊等功能。
  9. Design of variable - structure attitude control system for rlv reusable launch vehicle

    可重復使用運載器變結構姿態控制演算法設計
  10. 6. using simulation data of cz - 2f launch vehicle fault simulation system, the result of simulation based on cz - 2f launch vehicle pitch direction indicate that hm filtering fault detect can assure whether fault occurs, and this method achieves a better robustness and improves detect accuracy

    以cz ? zf大型運載火箭作為研究對象，利用c2 ? 2f運載火箭故障模擬系統的模擬數據，使用h _濾波故障檢測方法對cz ? 2f運載火箭的俯仰通道進行了故障檢測模擬，通過對余量曲線的分析表明這種方法能較好的判斷故障是否發生，由此說明了利用h _濾波理論進行魯棒故障檢測的可行性。
  11. Abstract : this paper presents a solved computation method fo r non - stationary random response subjected to excitation based on the theory of vehicle dynamics, launch dynamics and random vibration the dynamic and response characteristics of the selfpropelled gun launching duping travelling are studi ed, which is of value in structural design and practical operation of the system

    文摘:該文以車輛行駛動力學和火炮發射動力學理論為依據，利用隨機振動理論，提出了在隨機激勵下非平穩隨機響應的計算方法，並以某自行火炮為研究對象，用該方法探討了該系統在隨機路面上作行進間射擊時的動力特性和動態響應，對該類系統的結構設計和實際應用均有參考價值
  12. Ceramic thermal protection system for reusable launch vehicle

    地鐵供電系統設備選擇與全壽命周期費用的關系
  13. Abstract : physical and mathematical model for the inertial platform initialization align system of launch vehicle is discussed in this paper

    文摘:本文討論並建立了運載火箭初始對準系統的物理數學模型，並用多媒體手段對系統實際工作過程進行了模擬模擬。
  14. This paper has researched on the performances of heat transfer and flow in the heat exchanger, the collective vehicle project and the performance of launch system about this concept

    本文對這一概念中的換熱器內工質傳熱流動性能、運載器總體方案、發射系統性能等開展研究。
  15. At last the skeleton animation technique is used to realize “ walk ” effect of virtual people in the scene. these are part of the bases to realize the complete scene simulation system of launch vehicle

    以上所列出的視景模擬技術是整個火箭視景模擬系統的基礎，這些技術在該系統中得到了運用，效果較為理想。
  16. Temperature regulation system optimizing control for multi - function launch vehicle of certain missile

    某型導彈多功能發射車調溫系統的優化控制
  17. Independence power plant summarize of missile launch vehicle of a new certain weapon system

    某新型武器系統發射車主機發電設備綜述
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