例句與造句

1. Frame - oriented method on trajectory simulation
   面向框架的彈道仿真方法
2. Missile trajectory simulation based on increment proportional guide
   增量比例導引彈道仿真研究
3. Research on the whole flying trajectory simulation system of command guided antiaircraft missile
   指令制導防空導彈全彈道飛行仿真系統(tǒng)研究
4. As combat simulation frame and as missile trajectory simulation model are setup in the paper
   建立了空地作戰(zhàn)任務仿真框架和空地導彈的彈道計算模型。
5. 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)外導彈飛行特點的基礎上，進行空地導彈彈道仿真。
6. It's difficult to find trajectory simulation in a sentence. 用trajectory simulation造句挺難的
7. 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。
8. 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
   分析了空地導彈攻擊的彈道變化過程，將攻擊過程劃分為五部分，分別對各段建立了重心運動方程并進行了仿真，最后給出了空地導彈攻擊的全過程彈道仿真結果。
9. 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程空空導彈復合制導的兩種中制導律，即用于中程導彈的最優(yōu)預測比例導引中制導律和用于遠程導彈的奇異攝動中制導律，它們均有很好的中制導性能，能夠滿足中末制導的交班要求；接著研究了兩種末制導律，即用于被動雷達末制導的變結構制導律和用于主動雷達導引頭的最優(yōu)末制導律，均適用于復合制導末制導段；然后分析了中末制導的交班誤差源，討論了用于復合制導的交接律；最后通過仿真，驗證了提出的中制導律和末制導律，結合提出的交接規(guī)律，在不同的情況下對中末制導段彈道進行了仿真驗證，結果證明文中提到的中末制導律能夠達到性能指標要求。