近程導彈 的英文怎麼說
中文拼音 [jìnchéngdǎodàn]
近程導彈
英文
short-range missile- 近 : Ⅰ形容詞1 (空間或時間距離短) near; close 2 (接近) approaching; approximately; close to 3 (親...
- 程 : 名詞1 (規章; 法式) rule; regulation 2 (進度; 程序) order; procedure 3 (路途; 一段路) journe...
- 導 : 動詞1. (引導) lead; guide 2. (傳導) transmit; conduct 3. (開導) instruct; teach; give guidance to
- 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
- 近程 : short range近程彈道導彈 [軍事] short range ballistic missile; 近程導彈 [航空] short range missile...
- 導彈 : guided missile
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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。Under the circumstances of all - round blockade and embargo imposed by the united states and other western countries, china successfully developed intermediate and short - range missiles in 1964, and succeeded in launching its first man - made earth satellite in 1970, and a recoverable satellite in 1975
在美國等西方國家對中國實行全面封鎖和禁運的情況下, 1964年中國就已經研製成功了中近程導彈, 1970年中國成功地發射了第一顆人造地球衛星, 1975年,中國又成功地發射了返回式衛星。Then the judging method is proposed, and the proposed method can consider the stress history and viscosity shear strength of soft soil. in this paper, a fem program dpfbm1. 0 ( double plastic foundation beam method ( version 1. 0 ) ) is established. with this program, the influence of some parameters on foundation excavation is fully studied, the parameters include : compression modulus, cohesive strength, angle of internal ficiction, effective angle of internal friction, the embedded length of the wall and building load
針對當前國內外彈性地基梁法存在的缺陷,基於對軟土流變性的研究,採取了剪應力判斷彈塑性狀態,以改進和完善基坑工程彈性地基梁法,推導了彈性狀態下地基反力系數的近似解,提出了採用剪應力組合判斷土彈簧彈塑性狀態的方法,編制了相應的彈塑性共同變形法分析程序dpfbm1 . 0 ( doubleplasticfoundationbeammethod ( version1 . 0 ) ) ,並採用該程序分析了壓縮模量、粘聚力、內摩擦角等參數變化對基坑工程的影響。Without any foreign assistance, china has independently developed intermediate and short - range missiles, long - range rockets, submarine - launched solid - propellant rockets, recoverable satellites, the technology to launch multiple satellites atop a single rocket, and geostationary communication satellites
中國的中近程導彈、遠程火箭、潛艇水下發射固體燃料火箭、返回式衛星、一箭多星、地球靜止軌道通信衛星都是在沒有任何外國幫助下獨自完成的。Short - range attack missile
近程攻擊導彈They are classified as intercontinental, long - range, medium - range and short - range missiles
它們分別為洲際導彈、遠程導彈、中程導彈、近程導彈。Advanced short - range air - to - air missile
先進近程空對空導彈In this paper, the characteristic curves of diaphragm spring using nonlinear fem in ansys are consistent with the ones based on almen - laszlo formulae, and more adjacent with the experimental curves ; in addition, the simulation of diaphragm spring ' s stress change in working condition is described which provide the guidance of spring ' s design
摘要利用ansys對膜片彈簧進行非線性有限元分析得到的彈性特性曲線與經驗公式計算的曲線相當吻合,且更為貼近實驗曲線;同時對膜片彈簧的工作全過程的應力變化進行了模擬,以對膜片彈簧的設計提供指導。Research on the model of end mobile anti - ship missile penetrating anti - missile artillery
反艦導彈末端機動對近程反導艦炮的突防模型研究Those were short - range missiles. land - based
那是近程導彈,陸基的Recent satellite images show north korea fueling a long - range missile
最近的衛星圖像顯示,北韓正在為一枚遠程導彈裝填燃料。In order to study the behaviour of barrette pile group interaction and barrette pile group - soil - cap interaction, the proposed approximate three dimensional method of single pile is extended in this paper. the respective governing load - settlement equations corresponding to barrette pile group interaction and barrette pile group - soil - cap interaction have been derived
為了研究壁板樁群樁的相互作用和壁板樁群樁?土?承臺的共同作用,本文將壁板樁單樁的近似三維彈性理論法作了進一步延伸,分別推導出了各自的荷載沉降控制方程,並編制了相應的程序。This article uses foundation layered elastic modle which is analogy to the real project, deduces and solves the plate by boundary element method ( bem ) and summing in layers method
本文選用與實際工程場地特性較為接近的分層彈性地基模型,採用邊界元法推導並求解中厚板。To solve the resource problem of anti - missile radar omnidirectional and high data rate tracking targets, missile self - position technology to improve missile position precision based on the scheme of passive bd is put forward
摘要為了解決近程防空導彈制導雷達實現全方位、高數據率跟蹤多自標、截獲跟蹤多導彈遇到的資源緊張問題,提出了利用bd無源定位方案實現導彈自定位,提高導彈自定位精度的方法。Based on the basic equations of the elasticity plane problem, displacement fields and singular stress fields near the v - notch tip under mixed - mode of i and ii are obtained for homogeneous materials by a new definition of the stress intensity factors
基於彈性力學平面問題的基本方程,通過重新定義應力強度因子,推導了均質材料-復合型v型切口尖端附近的位移場和奇異應力場。Based on the basic equations of the elasticity plane problem and the two airy stress functions in the thesis, stress singularity eigenequations and displacement fields as well as singular stress fields near the v - notch tip and the crack tip for homogeneous materials are obtained
本文基於彈性力學平面問題的基本方程,引入兩個airy應力函數,推導了均質材料型切口尖端和裂紋尖端的應力奇異性特徵方程及其附近的奇異應力場和位移場。The pentagon ' s annual report to congress says the country ' s consistent defense spending on aircraft, missiles and ships means china is ever closer to a longer - range military reach
這份五角大樓致美國國會的年度報告說,該國家在戰機、導彈和軍艦上持續的國防花費意味著中國正在不斷地向遠程軍事打擊靠近。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分享友人