中英
1
trajectory-controlled中文是什么意思
- 中文翻譯
- 造句
- 彈道可控的
- trajectory n. (拋射體的)軌道，彈道；流軌；【幾】軌線。 a c ...
- control n. 1.支配，管理，管制，統(tǒng)制，控制；監(jiān)督。 2.抑制 ...
- trajectory n. (拋射體的)軌道，彈道；流軌；【幾】軌線。 a curved [direct-fire, flat, highangle fire, low] trajectory 曲射[直射、平射、高射、低射]彈道。
- controlled 被調(diào)節(jié)的; 管制的，被控制的; 可控的; 克制的; 受控的; 受控訪問性; 受控制的；受管制的；受節(jié)制的; 受約束的; 自制的
- abort trajectory 應急中斷飛行后的軌跡
- acceleration trajectory 加速軌道
- actual trajectory 實際彈道; 實際軌跡
- aeroballistic trajectory 空氣動力彈道學軌跡
- aerodynamic trajectory 空氣動力彈道; 氣動彈道
- air trajectory 空氣彈道; 空氣軌跡
- angle of trajectory 出手角度
- angular trajectory 角坐標彈道
- apex of the trajectory 彈道頂點
- apex of trajectory 彈道頂點
- arc of trajectory 彈道弧軌跡弧
- arching trajectory 弧形彈道
- arrival trajectory 抵達彈道
- ascending trajectory 上升軌跡
- assisted trajectory 利用空氣動力的飛行軌跡
- attack trajectory 攻擊彈道
- ballistic trajectory (火箭的)放射彈道。
- ballistic，trajectory 彈道
- base of trajectory 彈道基線; 基準彈道; 炮口水平面
- bit trajectory 鉆頭軌跡
- bomb trajectory 炸彈彈道
- At present , the most effective method of destroying the warhead of btm is the technology of directly hit kinetic kill , which can achieve precision control to the missile by adding the trajectory - control jet or attitude - control jet
目前對付來襲tbm彈頭最有效的手段就是采用直接碰撞動能殺傷技術(shù)。它是通過在導彈上安裝響應快速的雙組元軌、姿控發(fā)動機以實現(xiàn)對導彈的精確控制。 - The main works and achievements are described : ( 1 ) the application of direct lateral force on the exoatmosphere kinetic - kill vehicle . at first , the collectivity project of the exoatmosphere kinetic - kill vehicle is specified , the motive model of the exoatmosphere kinetic - kill vehicle and target are constructed , and the thrust performance of trajectory - control engine and attitude - control engine are presented
研究的內(nèi)容及成果主要表現(xiàn)在以下幾個方面： (一)直接側(cè)向力在大氣層外動能攔截器中的應用首先確定了動能攔截器的總體方案，分別建立目標運動和動能攔截器運動的數(shù)學模型，以及軌控和姿控發(fā)動機的推力模型。 - The main work and achievements are described as follows : ( 1 ) the analysis of the extra - atmospheric kinetic - kill vehicle at first , the motion model and dynamics model of the kinetic - kill vehicle is constructed , and the thrust performance of trajectory - control system and attitude - control system are presented , then the algorithms of realizing the guidance law , the methods of trajectory and attitude control are studied
研究內(nèi)容及成果主要表現(xiàn)在以下幾個方面： (一)大氣層外動能攔截器分析首先建立了動能攔截器運動學和動力學模型，以及軌控發(fā)動機和姿控發(fā)動機的推力模型，提出了攔截導引律的實現(xiàn)方法及軌控和姿控發(fā)動機的控制規(guī)律。 - The main works of this thesis are research of lateral force control and guidance of interceptors , emphasized on the terminal phase when intercepting the tactical ballistic missiles , including the performance analysis of extra - atmospheric kinetic - kill vehicle piloted by trajectory - control and attitude - control systems , and combined control of aerodynamics with lateral jets in atmosphere
本文主要研究攔截彈在攔截戰(zhàn)術(shù)彈道導彈時，末段的制導和側(cè)向力控制問題，包括大氣層外動能攔截器在姿控與軌控發(fā)動機作用下的性能分析，和大氣層內(nèi)側(cè)向力與氣動力復合控制研究。 - And then based on a surface - to - air missile that satisfies the requisition nearly , by means of reconstructing its geometry size , subsystems such as engine , the interceptor model used to continue the following studies is established . then the trajectory - control jet or attitude - control jet is added to the interceptor based on the analysis of the relationship between the missile performance and the thrust and configuration of the side jet
然后以基本滿足方案要求的某型防空導彈為基礎(chǔ)，對其幾何尺寸、發(fā)動機等分系統(tǒng)進行改進，并通過分析導彈性能與側(cè)噴發(fā)動機參數(shù)之間的關(guān)系，增加了姿控或軌控側(cè)向裝置，這樣得到了本文的研究工作所需的導彈模型。
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