控測火箭 的英文怎麼說

中文拼音 [kòngcèhuǒjiàn]
控測火箭 英文
sounding rocket
  • 控 : 動詞1 （告發;控告） accuse; charge 2 （控制） control; dominate 3 （使容器口兒朝下 讓裏面的液體慢...
  • 測 : 動詞1. （測量） survey; fathom; measure 2. （測度; 推測） conjecture; infer
  • 火 : fire
  • 箭 : 名詞（古代兵器） arrow
  • 火箭 : [航空] rocket; fire arrow; bird
  1. It is determined now by calculation with mathematical relationship of the flight thrust to the physical quantities which can be measured directly. the optimization of the software development platform is also analyzed inspect of the solid rocket - ramjet developmental program

    其次，為滿足固體火箭沖壓發動機試驗技術進一步研究需要，在深入分析labview圖形化編程軟體優化方法的基礎上，改進了現有的固體火箭沖壓發動機試驗測控程序，並應用於發動機試驗中。
  2. Rocket system refers to 225 modeling objects, and 75 single equipment ’ s models of control system and telemetry system were created in this thesis

    火箭箭上設備總計225個建模對象。本文分別創建了控制系統和遙測系統中的75個單機設備模型。
  3. The agency never determined the exact nature of the problem that delayed last week ' s launch but surmised it was caused by a locking pin in the rocket ' s flight control, which failed to retract before launch because ice had formed on it

    這次發射原本定在上周，美國宇航局還沒能確定導致發射被推遲的問題究竟為何，但推測問題可能出在火箭飛行控制系統的一個鎖定銷上。上周發射之前，因控制系統上結冰鎖定銷沒能縮回。
  4. Therefore, it is required to consider the visual effect and real - time performance of scene traveling when the 3d modeling is constructed. the elaborate model can be built by large numbers of polygons. but huge numbers of polygons would increase the scene processing time, and reduce the real - time performance of the scene

    火箭系統包括火箭箭體、控制系統、遙測系統、外安系統、利用系統、動力系統六大系統，模型多且結構復雜，創建三維模型時需要考慮到場景瀏覽的真實感與實時性。
  5. Changzheng long march 2f consists of ten subsystems : rocket body, control system, propulsion system, malfunctioning detection and management system, escape system, remote monitoring system, telemetry safety system, propellant utilization system, additional system and ground facilities

    運載火箭有箭體結構控制系統動力裝置故障檢測處理系統逃逸系統遙測系統外測安全系統推進劑利用系統附加系統地面設備等十個分系統。
  6. The research project of the middle - long and hypersonic missile with solid rocket - ramjet engine has been launched. the measurement and control technologies are the important basis of developing engine, which is one of the key technologies of the research

    我國發展中遠程、高超聲速固體沖壓導彈已經啟動，其關鍵技術之一是研製性能優良的固體火箭沖壓發動機，而試驗測控技術是發動機研製中不可或缺的重要基礎。
  7. Secondly, a new method on man - machine control is proposed. the axis - aligned bounding boxes arithmetic ( aabb ) and sphere area query arithmetic is applied to realize the collision effect of the virtual people in the launch vehicle testing hall

    其次，本文對人機交互控制提出了一種新的實現方法，漫遊時碰撞檢測則採用了軸向包圍盒法（ axis - alignedboundingboxes : aabb演算法）和球體區域查詢演算法來實現虛擬人物與火箭測試大廳內物體的碰撞效果。
  8. Under the base of the parameter characteristics of the engine thermodynamics and the air - inlet simulation, the measurement and control schemes are designed with virtual instrument technology

    本文在深入分析討論固體火箭沖壓發動機試驗參數特點以及進氣模擬對控制系統要求的基礎上，提出了發動機溫度、壓力、流量及其推力測量的總體方案和進氣模擬總體控制方案。
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