機上彈射器 的英文怎麼說

中文拼音 [shàngdànshè]
機上彈射器 英文
airborne catapult
  • : machineengine
  • : 上名詞[語言學] (指上聲) falling-rising tone
  • : 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
  • : Ⅰ動詞1 (用推力或彈力送出) shoot; fire 2 (液體受到壓力迅速擠出) discharge in a jet 3 (放出) ...
  • : 名詞1. (器具) implement; utensil; ware 2. (器官) organ 3. (度量; 才能) capacity; talent 4. (姓氏) a surname
  • 機上 : linux
  1. The high sensitive infrared detection and the telecamera with telescope are installed on the satellite. the infrared detection can detect the enemy missile ’ s infrared radiation and sound alert signal when the missile flies upward after it ’ s launched from on the surface or underwater

    衛星裝有高靈敏度的紅外探測和帶望遠鏡頭的電視攝像,在敵方從地面或水下發后數十秒內,紅外探測即可探測到導升段飛行期間發動尾焰的紅外輻,並發出警報。
  2. A mechanism for launching aircraft at a speed sufficient for flight, as from the deck of a carrier

    以適于飛行速度的發航空的一種械裝置,如從航空母艦的甲板
  3. New developments in decision theory, artificial theory and dynamic analysis method are applied to evaluation the possible projects. the main contents in this paper are included as follows : first, has improved an format reasoning method based on multiple attribute utility model and knowledgebase theory ; second, has proposed complex utility model by improving the theory of multiple attribute utility ; third, has presented a kind of weapon intelligent decision support system, based on the complex utility model and developed with com / dcom criterion ; forth, this paper also has build the dynamic simulation model for long - rang multiple tube rocket launcher system, and the tire dynamic model has applied in the rocket launcher system dynamic simulation model ; fifth, through building the rocket - launcher contact model, this paper has analyzed the dynamic forces between the rocket and launcher ; finally, this paper has build the evaluation model of the project about improving existing rocket launcher to the launcher that using canister, and get the conclusion through using the widss. the studies in this paper not only proposed scientific warrant to the choice of projects in this pre - studied national defense task about improving existing rocket launcher to the launcher that using canister, but also can give other studied tasks with decision supported

    主要內容包括:在總結決策分析與專家系統規則庫技術的基礎,提出了融決策分析與專家系統規則庫技術於一體的形式化推理制,該制能有效的將定量計算和定性知識融為一體,將規范的決策分析解題過程與專家系統特有的演化推理方法有結合起來;在多屬性效用理論的基礎,建立了一般形式的復式效用模型,並實用化了全相關乘式效用模型,提供了較完善的通用建模、分析和解釋功能:引入了com dcom組件技術,開發了基於組件的widss系統,該系統基於形式化推理制,易於擴展,能夠面向多種決策問題,具有較強的通用性;建立了遠程多管火箭炮全炮動力學模擬模型,將充氣輪胎動力學模型、輪胎和路面的相互作用模型運用於多管火箭炮動力學模擬計算中;利用碰撞接觸理論,對火箭在定向管內的運動受力情況進行了模擬計算;建立了遠程多管火箭炮箱式發改進方案模型,並利用動力學模擬計算結果在widss系統中進行了方案性能評估。
  4. This paper describes the development and trend of the weapon bay which the fighter plane equipped with at home and abroad, especially the missile ejection mechanism ; the kinematics and dynamics analysis about a sort of missile ejection mechanism is discussed and the model of the system is simulated by the tools in matlab, such as solver and so on

    本文在講述國內外飛艙,特別是導系統的發展現狀和發展趨勢的基礎,對現有引進的某型系統構進行了運動學和主要部件的動力學分析,並通過matlab提供的解算等工具對建立的系統模型進行了模擬。
  5. Firstly, this paper summarizes modern weaponry stealth technology at home and abroad, and lays special emphasis on analyzing stealth problem of cruise missile ’ s guidance head cover, aerocraft radar canopy and other privileged sites. secondly it makes a research on related theories of transparent metallic mesh that applied to missile ’ s guidance head cover and aerocraft radar canopy, and deduces relational expression between transparent metallic mesh structural parameters and radar wave - shielding efficiency, infrared transmitting. we use laser direct writing technique to fabricate a metallic mesh ( dimension : 70mm 70mm ; line width : 5 m ; period : 350 m ) on glass surface, then do experiment to test radar wave - shielding of metallic mesh via radar transmitting and receiving device

    本文首先綜述了國內外現代武系統隱身技術方法;重點對巡航導導引頭罩和飛雷達艙罩等特殊部位的隱身問題進行了研究,研究了金屬網柵用於導頭罩和飛雷達艙罩隱身的相關理論,推導了金屬網柵結構參數對雷達波屏蔽效率和透紅外關系式;用激光直寫工藝,在玻璃表面製作了一塊面積為70mm 70mm ,線寬為5 m ,線周期為350 m的金屬網柵;在實驗室里用雷達發和接收裝置測試了網柵對雷達波的屏蔽實驗;認為利用金屬網柵技術對雷達波具有一定的屏蔽作用,而且不影響精確制導的紅外線高效透過。
  6. Introduction : rambo has returned, and this will give us his interpretation of the worlds most elite special forces of the brilliant performance of the operation guide : keyboard control, moving from top to bottom and around key fire direction control, a key to machine guns, and grenades to the space bar, remember that there are weapons and ammunition restrictions oh, it should not an exaggeration to see a supplementary packet remember not miss 1, 10

    攻略:蘭博又回來了,這次他將給我們演繹全世界最精英的特種兵的精彩表現操作指南:鍵盤控制,下左右鍵移動並控制擊方向, a鍵為槍,而空格鍵為手雷,記得武都是有藥限制的哦,不要隨便亂用,看到了補充包就記得不要錯過咯
  7. Rambo has returned, and this will give us his interpretation of the worlds most elite special forces of the brilliant performance of the operation guide : keyboard control, moving from top to bottom and around key fire direction control, a key to machine guns, and grenades to the space bar, remember that there are weapons and ammunition restrictions oh, it should not an exaggeration to see a supplementary packet remember not miss 1, 10

    蘭博又回來了,這次他將給我們演繹全世界最精英的特種兵的精彩表現操作指南:鍵盤控制,下左右鍵移動並控制擊方向, a鍵為槍,而空格鍵為手雷,記得武都是有藥限制的哦,不要隨便亂用,看到了補充包就記得不要錯過咯
  8. In this paper, firstly, three - dimensional geometrical models of the target and ir flares are established and by using the software vega missile attacking process is real - time simulated visually. secondly, the ir radiation characteristic of the target, background and the ir flares are analyzed, in which the wave radiation of the sun at different time, wind speed, the relative humidity and ir radiation attenuation characteristic of the atmosphere is under consideration. from above the ir image of the target, ir flare and the background are got and then are normalized to gray color image that will be showed in a child window in real time

    本文通過三維建模工具creator建立目標、背景和干擾的三維模型,再通過視景模擬軟體vega生成載、導和目標飛的可見光場景圖像,實時地對導攻擊工程進行可視化模擬;並分析了目標、背景和干擾的紅外輻特性,計算出傳感路徑大氣衰減等等,將經過衰減的目標、背景和干擾的輻強度量化為灰度圖,以子窗口形式實時顯示;進一步可以使目標和干擾按照各自的運動軌跡運動,便可產生動態的紅外熱圖像序列。
  9. The results of simulation are analyzed in detail. the models which are established in the thesis are applicable to other style of missile. input parameters of engine, guiding rail, launch devices to model, you can gain the result what you need

    本文建立的模型對其它型號的導也適用,只需對導發動參數、定向有關參數、發架在艦艇布置參數和浪譜參數等輸入參數進行修改,就可得到不同型號導在發段的運動參數。
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