missile accuracy 中文意思是什麼
missile accuracy
解釋
導彈落點精度-
The jdam ( joint direct attack munition ) is a low - cost and high accuracy guidable bomb, owning to the laser guidable bomb have found many of disadvantages in the war. it is very important realistic and martial signification that we must develop the homing gliding missile though we are lacking in support from the finance
Jdam （聯合制導攻擊炸彈）是美軍針對第三代激光制導炸彈在戰爭中所暴露出來的各種缺點而研製的一種低成本、高精度的第四代制導炸彈，大力發展國產同類制導滑翔彈有重大的現實意義和軍事意義。 -
It is a more feasible method to realize the missile ’ s firing accuracy, by studying scene matching, track following, the middle guidance law and the terminal guidance law
比較可行的方法是抓住航跡規劃、航跡跟蹤、景象匹配、中制導和末制導等問題的研究，實現巡航導彈精確打擊目標。 -
Our country ' s cruise missile enterprise had a big disparity with the international advanced level, especially the missile ’ s firing accuracy, although had having the big development
我國巡航導彈事業雖已有了較大的發展，但與國際先進水平相比差距仍較大，尤其是導彈的射擊精度仍處于較低的水平。 -
Portable air defense missile as absolutely necessary weapon in air defense combat, may bring about the decrease of detection probability and guidance accuracy
便攜式地空導彈作為防空作戰中的必備武器，在受紅外干擾后，可能導致探測概率、制導精度的降低。 -
Simulation result showed that response time of missile was reduced and guidance accuracy was accordingly increased by side jet and aerodynamic compound control manner in terminal guidance
通過模擬研究表明：在末制導階段，採用燃氣動力氣動力復合控制方式可提高導彈的快速性，進而提高導彈的制導控制精度。 -
Many test cases are calculated to verify the above study. the cases are either real or standard testing models, including multi - element airfoil, wing - body configuration, cone / cylinder missile model and 3 - d high - lift systems, etc. the results of present calculation are in good agreement with experiment data, and show flexibility and accuracy of the approaches. base on the cartesian grids, this thesis has targeted the development and integration of many algorithms and techniques such as adaptive refinement, omni - tree data structure, hybrid grid method, etc. an analysis software and research methods are designed and developed for the steady - unsteady and viscous - inviscid flow complex systems and configuration
7 .運用上述研究成果和結論，進行了大量算例的實驗驗證，外形范圍包括多種標模與型號，涉及多段翼型、 m6機翼、細長體模型、翼身組合體、兩段機翼增升標模、帶縫翼和襟翼的三段增升翼身組合體等復雜外形，計算結果均與實驗吻合良好，充分說明了本文發展的各種演算法、流場求解、網格生成方法的正確性和魯棒性。 -
Mackenzie, donald. inventing accuracy : a historical sociology of nuclear missile guidance. cambridge, mass. : mit press, 1990
《創造精確性：關于核導彈制導的歷史社會學》 。 1990年麻州劍橋:麻省理工學院出版。 -
The cruise missile has the strong ability of the breakthrough defense, the high accuracy of hitting the target, the flexible agiligy, the easy implementaition in the technique and the low price in building etc., so it is welcome extensively by each country in the world, and has developed to become the important weapon in the modern war, and is one of the main combat targets after 90 ' s of last century
摘要巡航導彈具有突防能力強、命中精度高、靈活性強、技術上易於實現和造價低等優點而備受各個國家重視，已經發展成為現代戰爭的重要武器，是上世紀90年代以後的主要空中作戰目標之一。 -
It is obvious that the effectiveness of integrated missile and anti - aircraft gun weapon system is determined by its accuracy, capability, and so on
摘要針對彈炮結合防空武器系統毀傷概率是決定系統效能的關鍵問題，分析了決定系統精度和毀傷概率的主要因素及其相互關系。 -
The primary aim of this paper is that study the objects ’ detection possess random vein and lie to below the cloak - object. selecting ceramic tile image which possess random vein and presence cloak - objects, missile target image and jungle moving target image as study objects. mostly make research on matching algorithm " robustness and under this three strain circumstance matching algorithm " accuracy and it ’ s applicability
本文研究基於先驗知識的模糊遮掩物下的目標檢測問題，以具有隨機紋理且處于遮掩狀態的目標圖像為研究對象，實驗分析採用具有隨機紋理的瓷磚圖像、導彈目標的紅外圖像、叢林中移動目標圖像。 -
Based on analyzing the mechanism of direction finding triangulation location and location accuracy for two - ship passive locating, the acquisition probability model of anti ship missile terminal guidance radar is presented for two - ship passive locating : and the effects of the key factors to the probability are analyzed, and then the primary factors are pointed not by analyzing the results in different conditions
摘要首先簡要介紹了無源定位技術，然後著重分析了雙艦無源測向交叉定位以及其誤差產生的機理，在此基礎上，給出了雙艦無源定位情況下實施超視距攻擊時，反艦導彈末制導雷達開機時刻對目標的捕捉概率模型，並通過模擬分析雙艦距離。 -
In the modern aerial weapon experiment, especially missile testing experiment, the photoelectric theodolite is the main method that carries out the high - accuracy survey
在現代航空武器試驗中，尤其是導彈武器研製試驗中，光電經緯儀是進行高精度測量的主要手段。 -
Based on the small tactical missile system design, an engineering method for ram - air servo system dynamic accuracy analysis and verifying unit design is put forward
摘要從小型戰術導彈總體設計的角度提出了一種繼電控制沖壓式伺服系統的動態精度和校正裝置的工程分析和設計方法。 -
Application of uniform design to estimate autocontrol end - point scattering accuracy and hitting accuracy of anti - ship missile
反艦導彈自控終點散布和命中精度估算中均勻設計的應用 -
This experiential formula can be used in simulating steady condition, startup, acceleration work process and integrated design of cruise missile and turbofan engine so as to improve the accuracy of 1d engine performance computation
該經驗公式可用於彈用發動機穩態、起動、加速過程的計算和導彈與發動機一體化設計的數值模擬模型，從而提高發動機性能數值模擬的準確性。 -
The tactical missile seeker handover accuracy from midcourse to terminal guidance is researched. the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources. firstly, the terminal guidance seeker presetting parameters are computed, based on the equations of a surface - to - air missile movement and a target movement. then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed. it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target, which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided
研究復合制導的戰術導彈中末制導交班的導引頭預定精度問題.提出用小擾動法分析導引頭預定參數對誤差源的誤差敏感性關系.以中遠程防空導彈為例，結合導彈運動方程組和目標運動模型，計算了中末制導交班的導引頭預定參數，並計算了在制導站雷達測量誤差下的末制導導引頭預定參數的計算精度.可知，導引頭定位參數的計算誤差隨著彈目距離的接近而顯著增大，得到中末制導交班不能太晚的重要結論 -
Abstract : the tactical missile seeker handover accuracy from midcourse to terminal guidance is researched. the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources. firstly, the terminal guidance seeker presetting parameters are computed, based on the equations of a surface - to - air missile movement and a target movement. then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed. it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target, which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided
文摘:研究復合制導的戰術導彈中末制導交班的導引頭預定精度問題.提出用小擾動法分析導引頭預定參數對誤差源的誤差敏感性關系.以中遠程防空導彈為例，結合導彈運動方程組和目標運動模型，計算了中末制導交班的導引頭預定參數，並計算了在制導站雷達測量誤差下的末制導導引頭預定參數的計算精度.可知，導引頭定位參數的計算誤差隨著彈目距離的接近而顯著增大，得到中末制導交班不能太晚的重要結論
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