中英
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trajectory simulation中文是什么意思
- 中文翻譯
- 造句
- 飛行軌跡模擬
- trajectory n. (拋射體的)軌道，彈道；流軌；【幾】軌線。 a c ...
- simulation n. 假裝；模擬；裝病，裝瘋；【生物學(xué)】擬態(tài)，擬色。
- 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。
- abort trajectory 應(yīng)急中斷飛行后的軌跡
- acceleration trajectory 加速軌道
- actual trajectory 實(shí)際彈道; 實(shí)際軌跡
- aeroballistic trajectory 空氣動(dòng)力彈道學(xué)軌跡
- aerodynamic trajectory 空氣動(dòng)力彈道; 氣動(dòng)彈道
- air trajectory 空氣彈道; 空氣軌跡
- angle of trajectory 出手角度
- angular trajectory 角坐標(biāo)彈道
- apex of the trajectory 彈道頂點(diǎn)
- apex of trajectory 彈道頂點(diǎn)
- arc of trajectory 彈道弧軌跡弧
- arching trajectory 弧形彈道
- arrival trajectory 抵達(dá)彈道
- ascending trajectory 上升軌跡
- assisted trajectory 利用空氣動(dòng)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(zhǔn)彈道; 炮口水平面
- bit trajectory 鉆頭軌跡
- bomb trajectory 炸彈彈道
- boost trajectory 助推段彈道
- Frame - oriented method on trajectory simulation
面向框架的彈道仿真方法 - Missile trajectory simulation based on increment proportional guide
增量比例導(dǎo)引彈道仿真研究 - Research on the whole flying trajectory simulation system of command guided antiaircraft missile
指令制導(dǎo)防空導(dǎo)彈全彈道飛行仿真系統(tǒng)研究 - As combat simulation frame and as missile trajectory simulation model are setup in the paper
建立了空地作戰(zhàn)任務(wù)仿真框架和空地導(dǎo)彈的彈道計(jì)算模型。 - Analyzing to a stand off missile ' s flight characteristics , the as missile trajectory simulation is completed
在分析了典型防區(qū)外導(dǎo)彈飛行特點(diǎn)的基礎(chǔ)上，進(jìn)行空地導(dǎo)彈彈道仿真。 - Abstract : the digital simulation methods for maintaining the trajectory on a given manifold are presented . particularly , the norm conserving schemes are given for the solution of the system of the quaternion equations in the trajectory simulation of the vehicle
文摘:給出保持軌道在給定流形上的數(shù)字仿真方法，特別對(duì)飛行器軌道仿真中的四元數(shù)微分方程組的求解給出保范處理。 - Then we analyzed the change process of trajectory in air - to - ground missile attack , built the movement equations based on the center of gravity of every segment . in the end we gave the whole trajectory simulation result of air - to - ground attack
分析了空地導(dǎo)彈攻擊的彈道變化過程，將攻擊過程劃分為五部分，分別對(duì)各段建立了重心運(yùn)動(dòng)方程并進(jìn)行了仿真，最后給出了空地導(dǎo)彈攻擊的全過程彈道仿真結(jié)果。 - In this paper . the question of compound guidance about mid - long range air - to - air missle to be considered . the main contributions are as follows : first , two midcourse guidance laws are given . that is optimally predictable pn micourse guidance , which is suitable for middle range missle , and singularly perturbed midcourse guidance . which is suitable for long range missle guidance ; then two terminal guidance laws are given . that is variable structure guidance , which is suitable for passive radar guidance . and optimal guidance which is suitable for active radar guidance ; and then the error sourses of hand - off are researched , the hand - off law is given at the time ; fmally , the midcourse guidance laws and terminal guidance laws are tested by simulation , and the whole trajectory simulation are given through hand - off law , and the results are satisfied
主要工作如下：首先研究了用于中遠(yuǎn)程空空導(dǎo)彈復(fù)合制導(dǎo)的兩種中制導(dǎo)律，即用于中程導(dǎo)彈的最優(yōu)預(yù)測比例導(dǎo)引中制導(dǎo)律和用于遠(yuǎn)程導(dǎo)彈的奇異攝動(dòng)中制導(dǎo)律，它們均有很好的中制導(dǎo)性能，能夠滿足中末制導(dǎo)的交班要求；接著研究了兩種末制導(dǎo)律，即用于被動(dòng)雷達(dá)末制導(dǎo)的變結(jié)構(gòu)制導(dǎo)律和用于主動(dòng)雷達(dá)導(dǎo)引頭的最優(yōu)末制導(dǎo)律，均適用于復(fù)合制導(dǎo)末制導(dǎo)段；然后分析了中末制導(dǎo)的交班誤差源，討論了用于復(fù)合制導(dǎo)的交接律；最后通過仿真，驗(yàn)證了提出的中制導(dǎo)律和末制導(dǎo)律，結(jié)合提出的交接規(guī)律，在不同的情況下對(duì)中末制導(dǎo)段彈道進(jìn)行了仿真驗(yàn)證，結(jié)果證明文中提到的中末制導(dǎo)律能夠達(dá)到性能指標(biāo)要求。
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