deflection angle造句
造句與例句
手機版
- Application of matlab and computer graphics in calculating deflection angle of railway ' s curve
和計算機圖形學(xué)在鐵路曲線偏角計算中的應(yīng)用 - Comparison and design of two different deflection angle measurement system for a 2 dof laser scanner
兩種二維激光掃描器擺角測量方法的比較和實現(xiàn) - The characteristics of glass shell of large deflection angle super slim cpt are discussed in this paper , and the mechanism of super slim cpt are also analyzed
本文通過論述大偏轉(zhuǎn)角超薄型彩管的玻殼特點，解析彩管的超薄化機理。 - Meanwhile , such parameters as diffraction efficiency , deflection angle and driving power of device have been analyzed and computed theoretically
電極厚度以及器件的聲光衍射效率、偏轉(zhuǎn)角度、聲驅(qū)動功率等參數(shù)。最后是器件的制作。 - The zhengyu pkc type sprinkler pipe adopt aluminum tubing with large deflection angle quick assembles coupling use for complex landform transport water and sprinkle
Pkc型球接頭移動噴灌管道，采用薄壁高強鋁合金管，配套大偏角、鍍鋅鋼制球接頭，具有偏轉(zhuǎn)角度大，密封性能好，方便移動，快速安裝的特點。 - At the end , the vibration responses are displayed in polar diagram synthetically , in which the displacement , the static offset and the deflection angle of rotor could be shown altogether
提出用極坐標(biāo)表征轉(zhuǎn)子振動特性的方法，可以更直觀、全面地反映轉(zhuǎn)子的振動幅度、機動飛行時的靜態(tài)偏移以及偏擺角。 - The super slim cpt deals with two problems , one is to extend the deflection angle of electron beam and another is to minimize the length of glass shell , especially the length of funnel
摘要彩色顯像管的超薄型化涉及到兩方面的問題，其一是擴大電子束的偏轉(zhuǎn)角，其二是減小玻殼的長度，尤其是錐體玻殼的長度。 - Experimental results show that in the condition of rapid movement , smaller objects and larger deflection angles between camera and planar body , the algorithm could guarantee the tracking accuracy and robustness in a certain extent
實驗結(jié)果證明，在平板圖案發(fā)生快速運動以及目標(biāo)圖案較小或者平板與攝像機平面偏角較大的情況下，該算法能在一定程度上保證跟蹤的準(zhǔn)確度和健壯性。 - In terms of the minimum energy dissipation rate theory , the division angle and deflection angle formulas are derived and applications with some topography data of the pearl river delta waterway are introduced . finally , a 2 - d flow model in the orthogonal coordinates is established
本文從最小能耗率的原理出發(fā)，推導(dǎo)分汊河道的分流角、偏轉(zhuǎn)角計算的理論公式，以角度計算公式的變換形式推導(dǎo)分流比公式，并介紹了最小能耗率原理的一些其它應(yīng)用。 - Taking no account of the non - uniformity of the detector , this paper analyzed the performance of the traditional four - quadrant angle - measurement algorithm and two other algorithms in calculating the pitch angle and the deflection angle of the incident ray , and also compared the error curve of the pitch angle calculated by each algorithm in the full plane
摘要在不考慮探測器非均勻性影響的情況下，本文分析了傳統(tǒng)四象限測角算法和另外幾種算法在計算入射光的俯仰角和偏轉(zhuǎn)角時的性能，還比較了在整個平面內(nèi)各個算法得到的俯仰角的誤差曲面。 - It's difficult to see deflection angle in a sentence. 用deflection angle造句挺難的
- Second , by computing the trajectory of the missile and the method of analyzing cep , influences that the fighter ' s height , speed , pitch angle , the deflection angle between fighter and target , and the target moving characters make on the times of fighter attack and missile launch are deeply developed . third , by relating the motion of the missile and the fighter , the influences that fighter ' s dive angle and the deflection angle between fighter and target make on the attack field of the fighter are discussed in this paper when the fighter perform vertical and horizontal attack . criterion of attack effect is proposed focusing on attack time of the fighter , trajectory of the missile and destruction probability to the target
本文主要完成了以下幾個方面的工作：對導(dǎo)彈可發(fā)射區(qū)和飛機可攻擊區(qū)進行建模，通過對導(dǎo)彈彈道的仿真計算，并運用典型的圓概率偏差精度分析方法，詳細(xì)討論了飛機實施攻擊時，飛機的飛行高度h 、速度v 、俯仰角、與目標(biāo)的偏離角_ x及目標(biāo)運動特性等對飛機攻擊時機和導(dǎo)彈發(fā)射時機的影響；因此，將飛機和導(dǎo)彈結(jié)合起來，詳細(xì)研究了飛機在垂直平面和水平平面內(nèi)實施攻擊時，飛機俯沖角和與目標(biāo)的偏離角_ x對飛機的攻擊范圍的影響；以飛機實施攻擊的時間t 、彈道特性和對目標(biāo)的殺傷概率p來評判對地攻擊的效果；最后給出典型算例，通過對空地攻擊過程的仿真實現(xiàn)，對飛機飛行過載提出要求。 - According to purpose of the towed flight , a new trajectory consisting of taking off , climbing phase , level flight phase is presented with . trajectory pitch angle of the towing plane is optimized . according to the flight law of the towing plane , the fin deflection angle and amplification coefficient of particle - system trajectory of carrier rocket are designed , in order to realizing flight steadily of the carrier rocker
根據(jù)牽引飛行的目的，對載機應(yīng)用了“起飛?爬升?平飛”的變軌道飛行方案，同時對載機軌道的傾角、傾角變化規(guī)律進行優(yōu)選設(shè)計；再根據(jù)載機的飛行規(guī)律，對運載器質(zhì)點系軌道的舵偏規(guī)律及其放大系數(shù)進行了設(shè)計計算，實現(xiàn)運載器穩(wěn)定牽引飛行。 - Along with the progress of drilling technology , many new types of bha such as steering motor assembly , dropping assembly with eccentric bend sub , dropping assembly with flexible connection are developed based on common building , dropping and holding assemblies . for using these bha , a new mathematical model is put forward for 3d static analysis of these types of bha under small deflection . and its weighted residual solution is given . the mathematical model includes ( 1 ) differential equations ; ( 2 ) boundary conditions at drill bit , stabilizer , bend angle , diameter change , tangential point and borehole wall ; ( 3 ) lateral forces and deflection angles of bit . the software based upon this method runs well
為了更好地應(yīng)用各種新鉆具，建立了適用于對普通下部鉆具、導(dǎo)向鉆具、帶偏心彎接頭和柔性接頭的下部鉆具進行三維小撓度靜力學(xué)分析的數(shù)學(xué)模型，包括( 1 )微分方程； ( 2 )鉆頭、穩(wěn)定器、彎角、變截面、切點和井壁的邊界條件； ( 3 )鉆頭的側(cè)向力和鉆頭轉(zhuǎn)角.給出了該模型的加權(quán)余量解.用該方法編寫的軟件應(yīng)用效果良好
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