飛彈針 的英文怎麼說

中文拼音 [fēidànzhēn]
飛彈針 英文
pin missile
  • 飛 : Ⅰ動詞1 （鳥、蟲等在空中活動） fly; flit 2 （利用動力機械在空中行動） fly 3 （在空中飄浮遊動） fly...
  • 彈 : 彈名詞1. （彈子; 小球形的東西） ball; pellet 2. （內裝爆炸物, 具有破壞和殺傷能力的東西） bullet; bomb
  • 針 : Ⅰ名詞1 （縫衣物用的工具） needle 2 （細長像針的東西） needle like things 3 （針劑） injection; sh...
  • 飛彈 : 1 （有自動飛行設備的炸彈） missile; missile plane; fly bomb; doodlebug; flying bomb; buzz bomb2 ...
  1. As far as the system observation for accuracy evaluation of carrier rocket is concerned, there may exist different types of observed data and priors. heterogeneous information means that the different information describing the different characteristics of the same object. since all of the information is relevant to the same object, the fusion is possible. it is a key problem that how to fuse the heterogeneous information to obtain the better evaluation result. therefore, the different heterogeneous information and data is thoroughly studied, moreover, the mathematical description for information fusion of different parameter priors and data is constructed in this paper. based on their relationship between different parameters, indirect prior and observation data is transformed into prior in impact point observation space, which is fused with original prior by weight determined by maximum entropy rule to obtain the mixed posterior distribution. therefore, the test results can be given by combining posterior distribution and impact error observed data. then its application on evaluating guidance systematic error is elaborated as it applies trajectory tracking data, test value of coefficients of guidance instrumentation systematic error, impact point observation data and prior. especially, the advantage of this method lies in its application in case that guidance instrumentation systematic error may not be computed precisely. finally a detailed example on evaluation of carrier rocket is given to verify the theory

    為充分利用運載火箭觀測中的不同觀測空間和過程的信息來進行精度評估，針對該背景建立了異質先驗融合的數學描述.研究了飛行試驗中不同觀測空間和過程的異質先驗信息和數據，基於不同觀測過程的解析關系，將間接過程的先驗和觀測數據算出的后驗分佈轉換成落點觀測空間上的先驗，與原落點的先驗進行了最大熵加權融合，得到混合后驗分佈，從而結合落點觀測數據給出評定結果.在無法解算出精確的制導工具誤差系數的情況下，這種方法充分利用了彈道跟蹤數據、工具誤差系數的地面測試先驗值、落點先驗及落點數據，穩健性更好，準確性更高
  2. Two new algorithms, adaptive model and adaptive interacting multiple model, are presented in this paper with respect to the maneuvering trajectory characteristics of anti - ship cruisle missiles

    針對比例制導的飛航式反艦導彈彈道的特點和機動特徵，提出了跟蹤此類目標的兩種新演算法? ?基於自適應模型的演算法和基於自適應交互多模型的演算法。
  3. Next steps at the oecd are for countries to report to november and february working group meetings the actions they have taken in implementing these recommendations

    針對這個地區的飛彈威脅，我們建立先進的彈道飛彈防衛系統來保護美軍與盟邦。我們已在南韓部署改良式愛國者飛彈。
  4. Development of an antiradiation sam, most likely intended to target awacs aircraft and standoff jamming platforms

    研發一種反輻射面對空導彈，最有可能是針對awacs飛機和抵銷型干擾平臺。
  5. 1, the arrow next control around 2, y enable aircraft by clockwise or counterclockwise to 3. cache and the use of the space bar while firing bullets 4, only three lives

    箭頭控制上下左右x y使飛行器按順時針或逆時針轉向-和空格鍵同時使用發射子彈只有三條命。
  6. Aimed to solve problem of airdefence missile end control invalidation, a new idea of building direct lateral force control in terminal trajectory is presented, and the optimal action position, mode and range are analyzed

    （二）直接側向力在大氣層內防空導彈中的應用1 、針對防空導彈末端飛行失控問題，提出了建立末端直接側向力控制的新思路。對直接側向力最佳作用位置、最佳作用方式、最佳應用范圍進行了分析。
  7. This thesis mainly deal with the visualization simulation of missile flight. base on some basic concept of visualization simulation and some typical method as well as some simulation tools. a visualization simulation example of a kind of air - to - air missile was given in the thesis

    本文主要研究導彈飛行過程中的可視化模擬，在講述可視化模擬的一些基本概念、典型的可視化模擬方法和常見模擬工具的基礎上，針對某型號空空導彈，實現了其飛行過程可視化模擬。
  8. 6. utilizing the new robust decoupling control method which is put forward above, the design problem of decoupling controller for large angle of attack reentry missile ' s attitude control system is mainly investigated

    6 、針對大攻角再入飛行導彈通道間存在的氣動耦合現象，以及實際飛行中存在的個確定因素，分析了其進行解耦控制的必要性；探討了本文提出的基於互補靈敏度成形和h 。
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